Chapter 2

Laplace equation & Layer Potentials

The Laplace equation is perhaps the first elliptic PDE most people encounter. It is ubiquitous in the real world and for good reason! It describes physical states of harmony which can be seen using mathematical theorems on Harmonic functions. In real life, it can model steady state solutions of the heat equation, soap bubble films and electric voltage with no free electric charges. For us, the Laplace equation is a stepping stone to the Helmholtz equation. We discuss classical results on harmonic functions, to then prove the uniqueness of solutions to boundary value problems using the Laplace operator. Afterwards we discuss layer potentials in the Laplace equation setting to prove existence, and we note where the resulting second-kind formulations are well conditioned. These layer potentials are conceptually grounded using the electric voltage context, which is useful for the Helmholtz equation in our future. We then note what the smoothness assumptions on the boundary are actually buying us, and what changes at corners. Lastly, we study the spectrum of the Laplacian itself. This may look like a detour, but the interior eigenvalues are precisely the wave numbers at which the Helmholtz boundary integral formulations fail.

2.1 Harmonic Functions

Definition 2.1.1 (Harmonic functions).

A twice differentiable real-valued function \(u\), defined on domain \(D\subset\R^m\) is called harmonic if it satisfies Laplace's equation

\[\Delta u = 0,\qquad x\in D\]

We say that \(\Delta\) is the Laplacian, and let \(\vec n\) denotes the outward pointing unit normal vector on a curve, we write the normal derivative as \(\frac{\partial u}{\partial \vec n}(x)=\vec n(x)\cdot \nabla u(x)\). Most of the theory of harmonic functions utilize Green's theorems [2, 4]. The first and second Green's theorems are practically a reformulation of Gauss' divergence formula.

Theorem 2.1.2 (Green's First Theorem).

Let \(D\) be a bounded domain of class \(C^1\), \(\vec n\) denotes the outward pointing unit normal vector on \(\partial D\). For \(u\in C^1(\bar D)\) and \(v\in C^2(\bar D)\), we have

\[\int_D u\Delta v + \nabla u\cdot \nabla v~\mathrm{d}\Omega = \int_{\partial D}u\frac{\partial v}{\partial \vec n} ~\mathrm{d}\Gamma.\]

Theorem 2.1.3 (Green's Second Theorem).

Let \(D\) be a bounded domain of class \(C^1\), \(\vec n\) denotes the outward pointing unit normal vector on \(\partial D\). For \(u, v\in C^2(\bar D)\), we have

\[\int_D u\Delta v - v\Delta u ~\mathrm{d}\Omega = \int_{\partial D}u\frac{\partial v}{\partial \vec n}-v\frac{\partial u}{\partial \vec n} ~\mathrm{d}\Gamma\]

The second Green's theorem applied to an harmonic functions (with \(v\equiv 1\)), directly leads us to the corollary that harmonic functions observe net flux zero.

Corollary 2.1.4.

Let \(u\in C^2(D)\) be harmonic in \(D\), then

\[\int_{\partial D} \frac{\partial u}{\partial \vec n}~\mathrm{d}\Gamma = 0\]

To study harmonic functions we first find the Green's function to the Laplacian, or the fundamental solution to the Laplace equation [4].

Theorem 2.1.5 (The Fundamental Solution).

The function

\[\varphi(x,y):=\begin{cases} \cfrac{1}{2\pi}\ln\left(\cfrac{1}{|x-y|}\right),\qquad& d=2\\ \cfrac{\Gamma\left(\frac{d-1}{2}\right)}{(d-2)2\pi^{(d-1)/2}}\cfrac{1}{|x-y|^{d-2}},\qquad &d\geq 3 \end{cases} \tag{2.1}\]

defined \(\forall x\neq y\) in \(\R^m\) is called the fundamental solution of Laplace's equation. For fixed \(y\in \R6d\) it is harmonic in \(\R^m\backslash \{y\}\)

Proof.

As the two-dimensional setting is our focus, we only prove the case for \(d=2\). The difference for higher dimensions will be noted. The fundamental solution to Laplace's equation is given by

\[-\Delta \varphi = \delta(x-y), \qquad x\in\R^2, \tag{2.2}\]

with \(\delta\) the dirac delta distribution. Since the Laplacian is rotation invariant, The fundamental solution observes radial symmetry, i.e., we can go to polar coordinates and use the ansatz

\[\varphi(x,y) = \psi(r),\qquad \text{ with }r = |x-y|,\]

and have

\[\Delta \varphi = \psi'' + \frac{d-1}{r}\psi' = 0.\]

Solving for \(\psi'\) gives us \(\psi' = cr^{-(d-1)}\) such that for \(d = 2\),

\[\psi = c\ln(r) + b.\]

In settings that have dimension higher than 2, it is typically argues that constant \(b\) is set to zero for the purpose of decay at zero with infinity. In the two-dimensional setting, the fundamental solution does not decay, but has logarithmic growth at infinity. The convention is to also set \(b=0\) here due to physical relevance and the fact that for the purpose of BIE, this constant would integrate away. To find the constant \(c\), we integrate (2.2) over a ball centered at \(y\) with \(\epsilon\) radius, \(\mathbb{B}_\epsilon(y) := \{x\in\R^m~|~|x-y|<\epsilon\}\), \(\mathbb{B}_\epsilon\) in short,

\[\int_{\mathbb{B}_\epsilon }\Delta \varphi~\mathrm{d}\Omega= \int_{\mathbb{B}_\epsilon }-\delta(x-y)~\mathrm{d}\Omega.\]

By definition of the dirac delta distribution and Green's first Theorem 2.1.2, we have

\[\int_{\mathbb{B}_\epsilon }\Delta \varphi~\mathrm{d}\Omega = \int_{\partial \mathbb{D}_\epsilon} \vec{n}\cdot\nabla\varphi~\mathrm{d}\Gamma = -1.\]

On the surface \(\partial \mathbb{B}_\epsilon\), we have

\[\vec n = \frac{x-y}{\epsilon}\qquad\text{ and }\qquad\nabla \varphi = c \frac{x-y}{|x-y|^2} = \frac{c}{\epsilon^2}(x-y),\]

thus,

\[\int_{\partial \mathbb{D}_\epsilon} \vec{n}\cdot\nabla\varphi~\mathrm{d}\Gamma = c\int_{\partial \mathbb{D}_\epsilon} \frac{|x-y|^2}{\epsilon^3}~\mathrm{d}\Gamma = \frac{c}{\epsilon}\int_{\partial \mathbb{D}_\epsilon}~\mathrm{d}\Gamma=2\pi c.\]

The fundamental solution in the two-dimensional space is then found to be

\[\varphi = \frac{1}{2\pi}\ln\left(\cfrac{1}{|x-y|}\right).\]

As the name suggestions, \(\varphi\) is fundamental to any finding any solution to the Laplace equation in the setting of boundary value problems. The fundamental solution to the Laplace equation also allows us to evaluate a harmonic function through it's behavior at the boundary through Green's formula.

Corollary 2.1.6 (Green's formula).

Let \(D\) be a bounded domain and \(u\in C^2(\bar D)\) be harmonic in \(D\), then

\[u(x) = \int_{\partial D}\frac{\partial u}{\partial \vec n}(y)\varphi(x,y)-u(y)\frac{\partial \varphi}{\partial \vec n}(x,y)~\mathrm{d}s(y) \tag{2.3}\]

Now to work towards the goals of proving existence and uniqueness of the solution to BVPs with the Laplacian, we note a couple of theorems, the proofs are left to the reader and can be found in [4, 2].

Theorem 2.1.7.

Harmonic functions are analytic, i.e., each harmonic function has a local power series.

This theorem implicitly states that any harmonic functions is infinitely differentiable at any point \(x\in D\). This allows us to prove the following:

Theorem 2.1.8.

Let \(D\) be a bounded domain and \(u\in C^2(D)\cap C^1(\bar D)\) be harmonic in \(D\) s.t.

\[u=\frac{\partial u}{\partial \vec n}=0\qquad \text{ on }\Gamma,\]

for open subset \(\Gamma \subset \partial D\), then \(u\equiv 0\) in \(D\).

This then lead to the classic Mean Value Theorem [4].

Theorem 2.1.9 (Mean Value Theorem).

Let \(u\) be harmonic in an open ball \(B_r(x)\) and continuous in the closure \(\overline{B_r(x)}\), then

\[u(x) = \frac{1}{|B_r(x)|}\int_{B_r(x)}u~\mathrm{d}\Omega = \frac{1}{|\partial B_r(x)|}\int_{\partial B_r(x)}u~\mathrm{d}\Gamma.\]

In essence, this theorem state that the function value of a harmonic function \(u\) at \(x\) is equal to the average volume over \(B_r(x)\) and the mean over \(\partial B_r(x)\). This then leads us to the Maximum-Minimum principle [4, 2], which is vital to proving uniqueness of the solution to BVPs with the Laplacian.

Theorem 2.1.10 (Maximum-Minimum Principle).

A harmonic function \(u\) on a domain \(D\) cannot attain its maximum or minimum unless it's constant on \(D\).

Moreover, if \(u\) is harmonic in \(D\) and continuously extends in \(\bar D\), then \(u\) reaches its minimum and maximum on the boundary. The theory of harmonic functions can also be extend to different types unbounded domains. For the purpose of this survey, we are particularly interested in domains \(D^c=\R^m\backslash \bar D\) with \(D\) a bounded domain itself. We refer to \(D\) as the interior domain and \(\R^m\backslash \bar D\) as the exterior domain. The interior and exterior domain are shown in Figure 2.1.

DDCDCDC
Figure 2.1. Interior, \(D\), and exterior, \(D^C\) domain related to the C-curve

We can extend Green's formula to the unbounded domain by imposing behavior at infinity [3].

Theorem 2.1.11.

Assume that \(D\) is a bounded domain of class \(C^1\) with a connected boundary \(\partial D\), outward unit normal \(\vec n\) and let \(u\in C^2(D^c)\) be a bounded harmonic function, then

\[u(x) = u_\infty + \int_{\partial D}u\frac{\partial \varphi}{\partial \vec n}-\frac{\partial u}{\partial \vec n}\varphi~\mathrm{d}\Gamma,\]

for \(x \in D^c\) and some constant \(u_\infty\). For \(d=2\),

\[\int_{\partial D}\frac{\partial u}{\partial \vec n}~\mathrm{d}\Gamma = 0,\]

and at \(\infty\), for \(R\) sufficiently large enough:

\[u_\infty = \frac{1}{2\pi R}\int_{|y|=R}u(y)~\mathrm{d}s(y)\]

2.2 Laplace BVPs

We define four classical Laplace BVPs which are the combinations of interior/exterior with Dirichlet/Neumann boundary conditions [3, 2]. Solutions to these problems are shown in Figure 2.3.

Problem 2.2.1 (Interior Dirichlet Problem).

Find a function \(u\) that is harmonic in \(D\), continuous in \(\bar D\), and satisfies the Dirichlet boundary condition,

\[\begin{align*} -\Delta u = 0,&\qquad x\in D,\\ u = f,&\qquad x \in \partial D, \end{align*}\]

with \(f\) a given continuous function.

Problem 2.2.2 (Interior Neumann Problem).

Find a function \(u\) that is harmonic in \(D\), continuous in \(\bar D\), and satisfies the Neumann boundary condition,

\[\begin{align*} -\Delta u = 0,&\qquad x\in D,\\ \frac{\partial u}{\partial \vec n} = g,&\qquad x \in \partial D, \end{align*}\]

in the sense

\[\lim_{h\to^+0}\vec n(x)\cdot \nabla u(x-h\vec n(x))= g(x), \qquad x\in\partial D,\]

uniformly, with \(g\) a given continuous function.

Problem 2.2.3 (Exterior Dirichlet Problem).

Find a function \(u\) that is harmonic in \(D^C\), continuous in \(\bar D^C\), and satisfies the Dirichlet boundary condition,

\[\begin{align*} -\Delta u = 0,&\qquad x\in D^C,\\ u = f,&\qquad x \in \partial D, \end{align*}\]

with \(f\) a given continuous function and

\[u(x) = \begin{cases} \mathcal{O}(1),\qquad &d = 2,\\ o(1),\qquad &d \geq 3, \end{cases}\]

uniformly.

Problem 2.2.4 (Exterior Neumann Problem).

Find a function \(u\) that is harmonic in \(D^C\), continuous in \(\bar D\), and satisfies the Neumann boundary condition,

\[\begin{align*} -\Delta u = 0,&\qquad x\in D^C,\\ \frac{\partial u}{\partial \vec n} = g,&\qquad x \in \partial D, \end{align*}\]

and

\[u(x) = o(1)\]

uniformly. The solution \(u\) converges to the boundary in the sense

\[\lim_{h\to^+0}\vec n(x)\cdot\nabla u(x+h\vec n(x))= g(x), \qquad x\in\partial D,\]

uniformly, with \(g\) a given continuous function.

2.3 Solution Uniqueness

We state and loosely prove uniqueness statements of these four problems. It is emphasized that uniqueness of a solution means at most 1 solution exists.

Theorem 2.3.1.

The interior and Exterior Dirichlet problems, 2.2.1 and 2.2.3, have at most 1 solution.

Proof.

Assume multiple solutions exist and they are not unique. For the interior problem with Dirichlet boundary condition \(f\), take 2 solutions \(u_1,u_2\in C^2(D)\cap C^1(\bar D)\), then \(u=u_2-u_1\) is harmonic with boundary values \(u=0\) on \(\partial D\). Since \(u\) is constant on the boundary and it cannot attain it's maximum or minimum in \(D\), it must be constant by the Maximum-Minimum principle. As \(u\) extends continuously in \(\bar D\), we have that \(u\equiv 0\), thus \(u_1=u_2\). The exterior domain follows similar structure, but the behavior at infinity plays an important role.
If a solution to the interior/exterior Dirichlet Laplace problem exists, it is unique.

More interesting things happen when the problems do not have a unique solution, but the null-space of the problem is non-trivial, as is the case for the interior Neumann problems. For the purpose of the proof, we define parallel surfaces.

Definition 2.3.2 (Parallel surfaces).

Let \(D\) be a domain of class \(C^1\) and \(\vec n\) be the outward unit normal vector on the boundary. The parallel surface of \(\partial D\) is defined as

\[\partial D_h := \left\{z = x + h\vec n(x)~|~x\in \partial D\right\}\]

Theorem 2.3.3.

The interior Neumann problem, 2.2.2, have unique solutions up to a constant. The exterior Neumann problem, 2.2.4, has at most 1 solution.

Proof.

We first prove the result on the interior domain. Assume multiple solutions exists and are not unique. Let \(u_1\) and \(u_2\) be solutions to 2.2.2, let \(u=u_1-u_2\). The function \(u\) solve 2.2.2 with \(g\equiv 0\). Suppose \(u\) is not constant on \(D\), then there exists a set \(B\subset D\) s.t.

\[\int_{B}|\nabla u|^2~\mathrm{d}\Omega > 0.\]

Take \(h\) small enough such that \(B\subset D_{-h}\), then using Green's first theorem, we see that

\[\int_{B}|\nabla u|^2~\mathrm{d}\Omega \leq \int_{D_{-h}}|\nabla u|^2~\mathrm{d}\Omega = \int_{\partial D_{-h}}u\frac{\partial u}{\partial \vec n}~\mathrm{d}\Gamma.\]

Taking \(h\to0\), since \(u\in C^1(\bar D)\), i.e., we have that

\[0<\int_{B}|\nabla u|^2~\mathrm{d}\Omega\leq0,\]

A contradiction, therefore \(u\) is constant. No further restrictions are applied to \(u\), since \(\frac{\partial }{\partial \vec n}\) invariant to translations by a constant, \(u_1\) and \(u_2\) differ by a constant.
For the exterior problem, we can work through it similarly, yet \(u_\infty = 0\), since \(u=o(1)\). This acts as the constant value for \(u\), hence \(u_1\equiv u_2\). If a solution to the exterior Neumann Laplace problem exists, it is unique.

2.4 Solution Existence

The existence proofs are very informative, particularly for numerical methods to solving the Laplace equations through boundary integral equations [3, 9]. For the purpose of existence proofs, we first discuss layer potentials which play a vital role in BIE methods and the rest of this overview. Afterwards, solutions to the Laplace equations are found in terms of these layer potentials by looking at their behavior near the boundary of \(D\) from both sides.

2.4.1 Layer Potentials

We first define two integral operators vital to the rest of this survey [3, 8].

Definition 2.4.1 (Single- and double-layer operators).

Given a density function \(\tau\in C(\partial D)\), the integral operators

\[\mathcal{S}\tau = \int_{\partial D}s(\cdot,y)\tau(y)~\mathrm{d}s(y),\]

and

\[\mathcal{D}\tau = \int_{\partial D}d(\cdot,y)\tau(y)~\mathrm{d}s(y),\]

are called, respectively, the single- and double-layer operators. The single- and double-layer kernels are respectively defined as

\[s(x,y) = \varphi(x,y) = \frac{1}{2\pi}\ln\left(\cfrac{1}{|x-y|}\right)\]

and

\[d(x,y) = \frac{\partial \varphi}{\partial \vec n(y)}(x,y) = \frac{1}{2\pi}\frac{\vec{n}(y)\cdot(x-y)}{|x-y|^2},\]

with \(\varphi\) the fundamental solution. The double- and single-layer kernels on the C-curve with target \(x=0\) are shown in Figure 2.2.

lap fund sol
Figure 2.2. The single and double-layer kernel on the C-curve with target \(x=0\).

We can now define the single- and double layer potentials as

Definition 2.4.2 (Single- and double-layer potentials).

Given a density function \(\tau\in C(\partial D)\), we have

\[u(x) = [\mathcal{S}\tau](x),\]

is called the single-layer potential and

\[v(x) = [\mathcal{D}\tau](x),\]

is called the double-layer potential.

Using the Leibniz Integral Rule, we see that both the single- and double-layer potentials are harmonic functions on domain \(\R^m\backslash \partial D\). Since they are harmonic functions, there might exist specific density function(s) \(\tau\) such that \(u\) and \(v\) satisfy the Laplace BVPs with specific boundary data! Indeed we will prove for a class of boundary data, when a density function can be found, leading to boundary integral equations and the existence of solutions.
Before existence, we touch on how to interpret the single- and double-layer potentials through sources, targets and charges, common terminology in BIEs in scattering theory [9, 1]. The evaluate single-layer potential \(u\) at a target point \(x\), we approximate the single layer integral operator using a quadrature scheme

\[u(x) \approx \sum_{j}\varphi(x,y_j)\tau(y_j)w(y_j),\]

where \(w(y_j)\) includes quadrature weights and the geometry the boundary \(\partial D\). The value of \(u\) at a target point \(x\) is a sum of various charges coming from source points \(y_j\) with charge \(\varphi(x,y_j)\tau(y_j)w(y_j)\). Since, \(\varphi\) has a singularity when the target and source points are the same, we look at this asif there is a pole, the source points, that eradiates a charge and affects the value of \(u\) at the target point. For this reason, we also call the source point a monopole in this setting. The charge is determined on the distance between \(x\) and \(y_j\) through \(\varphi\) with a boundary \(\partial D\) dependent initial charge from \(w(y_j)\) and \(\tau(y_j)\) describes the charge coming from the value of \(u\) on the boundary itself \(\partial D\). This all combines to one charge coming from one monopole, the full value of \(u\) at the target point is then the sum of all source points with their respective charges. The true single-layer potential then describes the charges coming from an infinite amount of source points.
The double layer potential \(v\) at a target point \(x\) can also be approximated through a quadrature scheme,

\[v(x) \approx \sum_{j}\frac{\partial \varphi}{\partial \vec n(y_j)}(x,y_j)\tau(y_j)w(y_j).\]

To obtain a conceptual grasp, we also approximate the normal derivative through a finite difference formula, for example centered difference,

\[\frac{\partial \varphi}{\partial \vec n(y_j)}(x,y_j) \approx \frac{\varphi(x,y_j + h\vec n(y_j)) - \varphi(x,y_j - h\vec n(y_j))}{2h},\]

for \(h\) small. The approximation to the double-layer potential,

\[v(x) \approx \frac{1}{h}\sum_{j}\left[\varphi(x,y_j + h\vec n(y_j))\tau(y_j)w(y_j) - \varphi(x,y_j - h\vec n(y_j))\tau(y_j)w(y_j)\right],\]

can then be interpreted as the affect of two monopoles with charges working in opposite directions and scaled by \(h\), hence \(y_j\) is referred to as a dipole in this setting. The double-layer potential can be seen as vibrations.

2.4.2 Jump conditions

To use the single- and double-layer potentials to solve interior and exterior Laplace problems, a good grasp on the limiting behavior of \(u(x)\) and \(v(x)\) as \(x\) reaches a point on the boundary \(\partial D\). To do so, we first discuss the behavior of the double-layer kernel as \(x\) reaches a point on \(\partial D\) over \(\partial D\). Then we look at the behavior of the single- and double-layer potentials behavior coming from the interior and exterior domain.
Let \(\gamma:[0,L]\to \partial D:t\mapsto \gamma(t)\) be an arclength parametrization of \(\partial D\), \(x(s)=\gamma(s)\), \(y(t)=\gamma(t)\), and \(n(t)\) the outward normal, with Frenet relation \(\gamma''(t)=\kappa(t)\cdot n(t)\), where \(\kappa\) is the curvature of the boundary. We have \(L\) the arc length and \(|\gamma'|\equiv 1\). Taylor expanding the parametrization at \(t\),

\[\gamma(t+\varepsilon)-\gamma(t)=\varepsilon\,\gamma'(t)+\frac{\varepsilon^2}{2}\gamma''(t)+O(\varepsilon^3).\]

Since \(n(t)\cdot\gamma'(t)=0\), by definition, and \(n(t)\cdot\gamma''(t)=\kappa(t)\),

\[n(t)\cdot\big(x(s)-y(t)\big)=\frac{\varepsilon^2}{2}\kappa(t)+O(\varepsilon^3),\]

and

\[|x(t+\epsilon)-y(t)|^2= (x(t+\epsilon)-y(t))\cdot (x(t+\epsilon)-y(t)) = \varepsilon^2|y'(t)|+O(\varepsilon^3).\]

Therefore, since \(|\gamma'|\equiv 1\),

\[d(t+\epsilon,t)=\frac{1}{2\pi}\cdot\frac{\tfrac{\varepsilon^2}{2}\kappa(t)+O(\varepsilon^3)}{\varepsilon^2+O(\varepsilon^3)}.\]

Taking \(\epsilon\to 0\),

\[d(t,t) = \frac{\kappa(t)}{4\pi}.\]

The kernel has a removable singularity with the limit found. The single-layer kernel has no such limit. This difference leads us to the core engine of boundary integral equations, the jump of the double layer operator from the exterior domain to the interior domain [3]. First we prove Gauss' formula

Lemma 2.4.3 (Gauss' formula).

Let \(D\) be a bounded domain of class \(C^2\) and \(D^C:=\R^m\backslash \bar D\). We have that

\[p(x) = [\mathcal{D}1](x) = \int_{\partial D}\frac{\partial \varphi}{\partial \vec n(y)}(x,y)~\mathrm{d}s(y) = \begin{cases} -1, & x\in D\\ \frac{-1}{2},& x\in \partial D\\ 0, & x\in D^C \end{cases} \tag{2.4}\]

Proof.

For \(x\in D\), Green's formula shows

\[u = \int_{\partial D}\frac{\partial u}{\partial \vec n}\varphi - u\frac{\partial \varphi}{\partial \vec n}~\mathrm{d}\Gamma,\qquad\text{ for }x\in D.\]

Taking \(u\equiv 1\) shows the first case.
For \(x\in D^C\), Gauss' first theorem shows

\[\int_{D}u\Delta\varphi + \nabla u\cdot \nabla \varphi~\mathrm{d}\Omega = \int_{\partial D}u\frac{\partial \varphi}{\partial \vec n}~\mathrm{d}\Gamma.\]

Taking \(u\equiv 1\) and the fact that \(\varphi(x,y)\) is harmonic in \(y\) for \(x\not\in D\), shows

\[\int_{\partial D}\frac{\partial \varphi}{\partial \vec n}~\mathrm{d}\Gamma = 0\]

Lastly, taking \(x\in\partial D\) requires a little more work. Fix \(x\in\partial D\), let \(D_\epsilon:= D\backslash B_\epsilon(x)\), \(\partial \tilde{B}_\epsilon = \{y~|~|y-x|=\epsilon \& y\in D\}\) and \(\partial \tilde D_\epsilon = \{y\in\partial D~|~|x-y|>\epsilon\}\). From the previous result, we know that

\[\int_{\partial \tilde B_\epsilon}\frac{\partial \varphi}{\partial \vec n}~\mathrm{d}\Gamma + \int_{\partial \tilde D_\epsilon}\frac{\partial \varphi}{\partial \vec n}~\mathrm{d}\Gamma = \int_{\partial D_\epsilon}\frac{\partial \varphi}{\partial \vec n}~\mathrm{d}\Gamma = 0.\]

Since \(\partial \tilde D_\epsilon\to \partial D\) as \(\epsilon \to 0\), we find \(\int_{\partial \tilde B_\epsilon}\frac{\partial \varphi}{\partial \vec n}~\mathrm{d}\Gamma\) as \(\epsilon\to 0\). In the two-dimensional setting, since the boundary is assumed to be smooth, we have that \(\tilde B_\epsilon\) tends to the arc of a semi-circle. By parameterizing the arc semi-circle, we find that

\[\int_{\partial \tilde B_\epsilon}\frac{\partial \varphi}{\partial \vec n}~\mathrm{d}\Gamma = \frac{1}{2},\qquad\forall \epsilon>0\]

Therefore,

\[\int_{\partial \tilde D_\epsilon}\frac{\partial \varphi}{\partial \vec n}~\mathrm{d}\Gamma = -\frac{1}{2},\qquad \forall \epsilon.\]

Taking \(\epsilon\to 0\), we see that

\[\int_{\partial D}\frac{\partial \varphi}{\partial \vec n}~\mathrm{d}\Gamma = -\frac{1}{2}\]

WE now have all the tools to find the jump of the double layer potential [3, 8].

Theorem 2.4.4 (The double-layer potential jump).

For \(\partial D\) of class \(C^2\), the double-layer potential \(v\) with continuous density function \(\tau\) can be continuously extended from \(D\) to \(\bar{D}\) and from \(D^C\) to \(\overline{D^C}\) with

\[v_\pm(x) = \pm \frac{1}{2}\tau(x) + [\mathcal{D}\tau](x), \tag{2.5}\]

for \(x\in\partial D\), where \(v_{\pm}(x):= \lim_{h\to^+0}v(x\pm h \vec n(x))\).

Proof.

The proof is through the classical splitting technique. Fix \(x_0\in\partial D\), we have

\[\begin{align*} [\mathcal{D}\tau](x) &= \int_{\partial D}d(x,y)\tau(y)~\mathrm{d}s(y),\\ &= \underbrace{\int_{\partial D}d(x,y)(\tau(y)-\tau(x_0))~\mathrm{d}s(y)}_{\tilde v(x)} + \tau(x_0)p(x). \tag{2.22}\end{align*}\]

The rest of the proof depends on proving that \(\tilde v(x)\) is continuous in the normal direction over \(x_0\) and finding the value at \(x_0\). To this end, let \(x_h = x_0+h\vec n(x_0)\), \(\Gamma_\delta = \partial D\cap B_\delta(x_0)\) and \(\Gamma_\delta^C = \partial D\backslash \Gamma_\delta\). For \(y\in \Gamma_\delta^C\), \(d(x,y)\) is continuous in \(h\to 0\). If we thus show that the integral over \(\Gamma_\delta\) vanishes uniformly in \(h\), we have shown that \(\tilde{v}\) is continuous.
Without loss of generality, let \(x_0 = 0\) and \(\vec n(x_0)=(0,1)^T\) (shift and rotation invariances), approximate the tanget line with \((s,g(s))\) where \(g(0) = 0\) and \(g'(0) = 0\). Since \(\partial D\) is of the class \(C^2\), we find through Taylor approximations that \(g(s) = \frac{1}{2}\kappa(0)s^2 + \mathcal{O}(s^3)\), where \(\kappa(0)\) is the curvature. Therefore we can bound \(g\) for \(s\) near 0,

\[|g(s)|\leq C|s^2|\text{ and } |g'(s)|\leq C|s|.\]

Now take \(x = (0,h)\), on the tangent and \(y\) goes over \((s,g(s))\) as \(\Gamma_\delta\) takes \(\delta\to 0\). We then have

\[x-y = (-s,h-g(s)),\Rightarrow |x-y|^2 = s^2+h^2-2hg(s) + g(s)^2 = s^2+h^2+\mathcal{O}(s^2h+s^4).\]

Therefore,

\[\vec n(y) = \cfrac{(-g'(s),1)}{\sqrt{1+g'(s)^2}} \Rightarrow \vec n(y)\cdot(x-y) = \cfrac{sg'(s)-g(s)+h}{\sqrt{1+g'(s)^2}}.\]

Since \(sg'(s)-g(s) = \mathcal{O}(s^2)\) and \(1+g'(s)^2=1+\mathcal{O}(s^2)\), we have that

\[\vec n(y)\cdot(x-y) = h +\mathcal{O}(s^2).\]

Under the assumption that the density function \(\tau\) is Hölder continuous, which is typically granted for (piecewise) smooth kernels,

\[\underbrace{|\tau(y)-\tau(x_0)| \leq L|y-x_0|^\alpha}_{\text{H\"older Continuity}} = L\left(\sqrt{s^2+g^2(s)}\right)^\alpha\leq \tilde{L}|s|^\alpha,\]

we have that

\[\frac{|\vec n(y) \cdot (x-y)|}{|x-y|^2}|\tau(y)-\tau(x_0)|\leq \frac{|h|+Cs^2}{s^2+h^2}|s|^\alpha.\]

Plugging this into the integral over \(\Gamma_\delta\), gives us

\[\int_{\Gamma_\delta} \frac{|\vec n(y) \cdot (x-y)|}{|x-y|^2}|\tau(y)-\tau(x_0)|\mathrm{d}s(y)\leq \int_{|s|\leq\delta}\frac{h+Cs^2}{s^2+h^2}|s|^\alpha~\mathrm{d}s,\]

where

\[\int_{|s|<\delta}\frac{h}{s^2+h^2}|s|^\alpha~\mathrm{d}s\leq \delta^\alpha\int_{-\infty}^\infty\frac{h}{s^2+h^2}~\mathrm{d}s = \pi\delta^\alpha,\]

and

\[\int_{|s|<\delta}\frac{Cs^2}{s^2+h^2}|s|^\alpha~\mathrm{d}s\leq C\int_{-\delta}^\delta|s|^\alpha~\mathrm{d}s = \frac{2C}{2+\alpha}\delta^{1+\alpha}.\]

Therefore,

\[\int_{\Gamma_\delta} \frac{|\vec n(y) \cdot (x-y)|}{|x-y|^2}|\tau(y)-\tau(x_0)|~\mathrm{d}s(y) \leq \tilde{C}\delta^\alpha,\]

uniformly in \(h\), thus \(\tilde v(x_h)\stackrel{h \to 0}{\to}\tilde v(x_0) \). We now find this \(v(x_0)\) and show the prove the statement. Use the Gauss' formula (2.4), we know that \(p(x_0)=\frac{-1}{2}\), thus from (2.22) we know that

\[[\mathcal{D}\tau](x_0) = v(x_0) = \tilde v(x_0) - \frac{1}{2}\tau(x_0) \Rightarrow \tilde v(x_0) = v(x_0) + \frac{1}{2}\tau(x_0) = \frac{1}{2}\tau(x_0) + [\mathcal{D}\tau](x_0).\]

We also know from the Gauss' formula the limiting behavior, i.e.,

\[v_+(x_0) = \lim_{h\to^+0}v(x_h) = \tilde v(x_0) + 0\tau(x_0)=\tilde v(x_0),\]

and

\[v_-(x_0) = \lim_{h\to_-0}v(x_h) =\tilde v(x_0) -\tau(x_0).\]

This leads us to and equation that will be used later,

\[v_+(x) - v_-(x) = \tau(x)\qquad\text{ for }x \in\partial D, \tag{2.6}\]

and the statement in the theorem,

\[v_+(x_0) = \frac{1}{2}\tau(x_0) + [\mathcal{D}\tau](x_0),\]

and

\[v_-(x_0) = \frac{1}{2}\tau(x_0) + [\mathcal{D}\tau](x_0) - \tau(x_0) = -\frac{1}{2}\tau(x_0) + [\mathcal{D}\tau](x_0).\]

For the single layer potential, no jump occurs due to the weak singularity. However, it can be used for the interior/exterior Neumann problems. Let \(u(x) = [\mathcal{S}\tau](x) \), we then have that

\[\frac{\partial }{\partial \vec n(x)}u(x) = \frac{\partial }{\partial \vec n(x)}[\mathcal{S}\tau](x) = \int_{\partial D}\frac{\partial }{\partial \vec n(x)}\varphi(x,y)\tau(y)~\mathrm{d}s(y).\]

We define the integral operator to be the adjoint of the double layer potential,

\[\mathcal{D}'\tau = \int_{\partial D}\frac{\partial }{\partial \vec n(\cdot)}\varphi(\cdot,y)\tau(y)~\mathrm{d}s. \tag{2.7}\]

Note that this is an adjoint w.r.t. the bilinear inner product \(\langle\cdot,\cdot\rangle\), and it itself is not a layer potential since it cannot satisfy any Laplace equation. However, similar jump conditions are observed, making them useful for the Neumann problems. Given \(u(x) = [\mathcal{S}\tau](x) \), we can prove

\[\frac{\partial u_+}{\partial \vec n(x_0)}(x_0) = -\frac{1}{2}\tau(x_0) +[\mathcal{D}'\tau](x_0) , \tag{2.8}\]

and

\[\frac{\partial u_-}{\partial \vec n(x_0)}(x_0) = +\frac{1}{2}\tau(x_0) + [\mathcal{D}'\tau](x_0). \tag{2.9}\]

This jump is special to the usage of the single layer potential. The jump condition of the double-layer operator does not survive the normal derivative and thus no jump condition is seen for the double-layer potential. In particular,

\[\frac{\partial v_+}{\partial \vec n} - \frac{\partial v_-}{\partial \vec n} = 0\qquad\text{ on }\partial , \tag{2.10}\]

On the other hand for the single layer potential, since it observes no jump we have that

\[u_+ - u_- = 0\qquad\text{ on }\partial , \tag{2.11}\]

However, the normal of the single layer potential does observe this jump. Using (2.8) and (2.9), we get

\[\frac{\partial u_+}{\partial \vec n} - \frac{\partial u_-}{\partial \vec n} = -\tau\qquad\text{ on }\partial D, \tag{2.12}\]


In the interest of future endeavors, we mention two facts on these kernels and future similar kernels [8].
First, we note that if \(\partial D\) is of the class \(C^2\), there exists an constants \(L_1\) and \(L_2\), s.t.,

\[|\vec n(x)\cdot (x-y)|\leq L_1|x-y|^2 \text{ and } |\vec n(x) - \vec n(y)|\leq L_2|x-y|,\]

which is seen through Taylor approximations where \(L_1\) and \(L_2\) are similar to the curvature. This can then be used to see that the double-layer kernel is weakly singular in dimension \(d\geq 2\),

\[|d(x,y)| \sim \frac{|\vec n(x)\cdot (x-y)|}{|x-y|^d}\leq \frac{\tilde L}{|x-y|^{d-2}}\text{ for }x,y\in\partial D,\]

hence \(\mathcal{D}\), and \(\mathcal{D}'\) are compact operators! It is trivial to see that the single layer kernel is also weakly singular and hence \(\mathcal{S}\) is also a compact operator.
Second, with scattering problems in sight, in particular with the Helmholtz equation, we have to note that the fundamental solution to the Helmholtz equation has similar singular behavior at \(|x-y|\to 0\), therefore these jump conditions will translate to the Helmholtz equation with new fundamental solutions.

2.4.3 Solutions through BIEs

The limiting behavior to the boundary now allows to us to reformulate the PDE into a BIE. For the Dirichlet Laplace problems we will be using the jump conditions described in Theorem 2.4.4. For the Interior Dirichlet problems (2.2.1) with boundary condition \(u=f\) on \(\partial D\), we have

\[\begin{align*} &u(x) = [\mathcal{D}\tau](x), \qquad& x\in D,\\ &\left[\left(-\frac{I}{2}+\mathcal{D}\right)\tau\right](x) = f(x), \qquad& x\in\partial D. \end{align*} \tag{2.13}\]

For the Exterior Dirichlet problem (2.2.3) with boundary condition \(u=f\) on \(\partial D\), we have

\[\begin{align*} &u(x) = [\mathcal{D}\tau](x), \qquad& x\in D,\\ &\left[\left(\frac{I}{2}+\mathcal{D}\right)\tau\right](x) = f(x), \qquad& x\in\partial D. \end{align*} \tag{2.14}\]

We can also reformulate the Neumann problems to BIEs using the jump conditions (2.9) and (2.8). For the Interior Neumann problem (2.2.2) with boundary condition \(\frac{\partial u}{\partial \vec n}=g\) on \(\partial D\), we have

\[\begin{align*} &u(x) = [\mathcal{S}\tau](x), \qquad& x\in D,\\ &\left[\left(\frac{I}{2}+\mathcal{D}'\right)\tau\right](x) = g(x), \qquad& x\in\partial D. \end{align*} \tag{2.15}\]

For the Exterior Neumann problem (2.2.4) with boundary condition \(\Dn u=g\) on \(\partial D\), we have

\[\begin{align*} &u(x) = [\mathcal{S}\tau](x), \qquad& x\in D,\\ &\left[\left(-\frac{I}{2}+\mathcal{D}'\right)\tau\right](x) = g(x), \qquad& x\in\partial D. \end{align*} \tag{2.16}\]

If we are able to find the density layer function, we are able to find solutions to the Helmholtz equation and thus prove the existence of solutions to the Helmholtz equation. To this end, we have to be able to invert operators like \(\pm\frac{I}{2}+\mathcal{D}\) and \(\pm\frac{I}{2}+\mathcal{D}'\). There are ”direct“ boundary integral formulations that, given Dirichlet boundary data, find Neumann boundary data to then use the Green's formula (2.3). For example, for the Dirichlet problem, we find the Neumann boundary data through

\[\int_{\partial D}s(x,y)\frac{\partial }{\partial \vec n(y)}u(y)~\mathrm{d}s(y) = \frac{1}{2}f(x) + \int_{\partial D} d(x,y)f(y)~\mathrm{d}s(y),\qquad x\in\partial D, \tag{2.17}\]

or given Neumann boundary data, we find the Dirichlet boundary data through

\[\frac{1}{2}u(x) + \int_{\partial D}d(x,y) u(y)~\mathrm{d}s(y) = \int_{\partial D}s(x,y) g(y)~\mathrm{d}s(y). \tag{2.18}\]

While the two do not need to an extra density functions \(\tau\), which comes with it's extra problems, we instead compute the other boundary data. However, an operator is still needs to be inverted and evaluated. In particular, here we must invert a compact operator, or Fredholm integral equation of the first kind \(\mathcal{S}\Dn u\). On the other hand, since \(\mathcal{D}\) and \(\mathcal{D}'\) are compact operators, we have that \(\pm\frac{I}{2}+\mathcal{D}\) and \(\pm\frac{I}{2}+\mathcal{D}'\) Fredholm integral equations of the second kind on which we are able to apply the Fredholm alternative!

Theorem 2.4.5.

Let \(\mathcal{D}\) and \(\mathcal{D}'\) be the double-layer operator and adjoint to the double-layer operator, respectively, then

\[\mathcal{N}\left(-\frac{I}{2}+\mathcal{D}\right) = \mathcal{N}\left(-\frac{I}{2}+\mathcal{D}'\right) = \{0\},\]

and

\[\mathcal{N}\left(\frac{I}{2}+\mathcal{D}\right) = \text{span}\{1\}\text{ and }\mathcal{N}\left(\frac{I}{2}+\mathcal{D}'\right) =\text{span}\{\psi_0\},\]

with

\[\int_{\partial D}\psi_0~\mathrm{d}\Gamma = 1\]

Proof.

Let \(\tau\) exist s.t. \(\left(\frac{I}{2}+\mathcal{D}\right)\tau \equiv 0\). We then know that the double-layer potential with this density function, \(u=\mathcal{D}\tau\), is harmonic. Using the behavior at the boundary found in Theorem 2.4.4, we know that

\[u_- \equiv \left(-\frac{I}{2}+\mathcal{D}\right)\tau\equiv 0.\]

By the uniqueness of the interior Dirichlet problem, we then have that \(u(x) = 0\) for \(x\in D\), hence \(\frac{\partial u_-}{\partial \vec n}\equiv0\). Since (2.10), we have that \(\frac{\partial u_+}{\partial \vec n}\equiv0\) which now corresponds to the exterior Neumann problem. Due to uniqueness of the exterior Neumann solution, we know that \(u\equiv 0\) for \(x\in D^C\), therefore, \(u_+\equiv0\). Therefore, because of the jump condition of the double-layer potential (2.6), we have that

\[\tau = u_+-u_- = 0,\]

hence the operator \(-\frac{I}{2}+\mathcal{D}\) is injectivity and due to the Fredholm alternative, it is invertible. Moreover, because of the Fredholm alternative,

\[\mathcal{N}\left(-\frac{I}{2}+\mathcal{D}\right) = \mathcal{N}\left(-\frac{I}{2}+\mathcal{D}'\right) = \{0\},\]

On the other hand, for the operator \(\frac{I}{2}+\mathcal{D}\), we solve the exterior Dirichlet problem, for which we again can use the uniqueness property. However, to use (2.6) again, we need the solution to the interior Neumann problem to be unique. We in fact know it is not and solutions differ by a constant. Hence

\[\mathcal{N}\left(\frac{I}{2}+\mathcal{D}\right) = \text{span}\{1\}.\]

The Fredholm alternative then also tells us

\[\mathcal{N}\left(\frac{I}{2}+\mathcal{D}'\right) = \text{span}\{\psi_0\},\]

with

\[\int_{\partial D}\psi_0~\mathrm{d}\Gamma = 1,\]

due to \(\mathcal{D}'\) being the adjoint of \(\mathcal{D}\) w.r.t. the bilinear inner-product.

The invertibility of the first two integral operators now proves existence of the solution to the interior Dirichlet problem and exterior Neumann problem. This alongside the uniqueness proofs, proves that interior Dirichlet problem and exterior Neumann problem have unique solutions. While this seems like a convoluted way to prove existence of solutions, it also gives us a very nice reformulation that can be exploited for numerical computations, as we will see in later chapters. In particular, we will numerically invert a Fredholm integral operator of the second kind, which comes with well-conditioned matrices [7, 9].
While the other operators are not injective, it does not mean there exists no solution to the associated problems! Instead, we use a different BIE, in particular a combination of the double- and single-layer operators.

Theorem 2.4.6 (“Modified” double layer potential).

Let \(D\subset\R^m\), be a bounded domain with \(y_0\in D\) and \(D^C = \R^m\backslash \bar D\),

\[u(x) = \underbrace{\int_{\partial D}(d(x,y)+s(x,y_0))\tau(y)~\mathrm{d}s(y)}_{[\mathcal{K}\tau](x)},\qquad x\in D^C \tag{2.19}\]

with \(\tau \in C\) s.t.

\[\frac{\tau(x)}{2}+ [\mathcal{K}\tau](x)= f(x),\qquad x\in\partial D,\]

is a solution to the exterior Dirichlet problem.

Proof.

Without loss of generality, assume \(y_0 = 0\) with a translated domain. To prove this, we prove the invertibility of the operator \(I/2 + \mathcal{K}\). First note that the kernel \(d(x,y)+s(x,y)\) is weakly singular when \(x=y\), therefore \(\mathcal{K}\) is a compact operator and thus \((I/2 + \mathcal{K})\) is a Fredholm integral operator of the second kind. Since \(\mathcal{D}\) is compact, \(\mathcal{K}-\mathcal{D}\) is compact and therefore continuous. Let \(\tau\in C\) s.t. \((I/2 + \mathcal{K})\tau=0\), \(u = \mathcal{K}\tau\) solve an exterior Dirichlet problem and

\[u_+ = \left(\cfrac{I}{2} + \mathcal{K}\right)\tau = 0\text{ on }\partial D,\]

therefor \(u\equiv 0\) in \(D^C\). Since \(d(x,y)/s(x,0)\to 0\) as \(|x|\to \infty\), we have

\[(s(x,0))^{-1}u \to \int_{\partial D}\tau(y)~\mathrm{d}s(y), \text{ as }|x|\to \infty,\]

therefore

\[\int_{\partial D}\tau(y)~\mathrm{d}s(y) = 0.\]

Moreover, from the boundary we know

\[(s(x,0))^{-1}u_+(x) =\frac{1}{2}(s(x,0))^{-1}\tau(x) + (s(x,0))^{-1}[\mathcal{D}\tau](x) + (s(x,0))^{-1}[(\mathcal{K}-\mathcal{D})\tau](x),\]

and we see that

\[(s(x,0))^{-1}[(\mathcal{K}-\mathcal{D})\tau](x) = \int_{\partial D}\tau(y)~\mathrm{d}s(y) = 0,\]

therefore,

\[(s(x,0))^{-1}\left(\frac{1}{2} + \mathcal{D}\right)\tau = 0 \Rightarrow \left(\frac{1}{2} + \mathcal{D}\right)\tau = 0.\]

From Theorem 2.4.5, we now know that \(\tau \in\text{span}\{1\}\), yet since \(\int_{\partial D}\tau\mathrm{d}\Gamma=0\), we have that \(\tau\equiv 0\) and thus \(I/2 + \mathcal{K}\) is injective. By the Fredholm alternative, \(I/2 + \mathcal{K}\) is invertible and therefore (2.19) exists and is a solution to the exterior Dirichlet problem.

Lastly, we mention that the interior Neumann problem is solvable iff \(\int_{\partial D}g~\mathrm{d}\Gamma = 0\) [3]. The necessary condition is a results from applying Green's first theorem. The exterior Neumann problem always has a unique solution in \(\R^3\) and has a unique solution in \(\R^2\) iff \(\int_{\partial D}g~\mathrm{d}\Gamma = 0\) due to the behavior of the fundamental solution at infinity. Solutions using the boundary integral equations is shown in Figure 2.3.

lap int dir
lap ext dir
lap int neu
lap ext neu
Figure 2.3. Solutions to Laplace boundary value problems. The exterior problems have boundary condition \(\sin(5s)\) for \(s\in[0,2\pi)\) and the interior problems have a source point (green dot) inside the domain.


Lastly we mention the following theorem showing continuous dependence on the boundary.

Theorem 2.4.7.

Solutions to the Dirichlet and Neumann problem depends continuously in \(\|\cdot\|_\infty\) on the given boundary data.

2.4.4 Notes on non-smooth domains

Throughout the section it is always assumed that the boundary is smooth enough, i.e., \(\partial D\) is of class \(C^2\). This can be extended to Lyapunov boundaries without much change in the prevvious discussions, i.e.,

\[\forall x\in \partial D,~\vec n(x)\text{ exists and }\vartheta(x,y)=\angle(\vec n(x),\vec n(y)) \text{ has } L,\alpha \text{ s.t. } \vartheta(x,y)\leq L|x-y|^\alpha.\]

However, many geometries of interest have corners (rectangles, triangles, keyholes, microwaves, ...) or cusps (teardrops, cardioids or manifolds with pitched ends, ...) [1, 8]. We will not work the BIE linked to these geometries out, but these corners and cusps have major consequences. For one, the section of the boundary inside a shrinking ball centered at the corner will no-longer go to a semi-circle as \(\epsilon\to 0\). This is relevant for the proof of Lemma 2.4.3. Moreover, the curve's parametrization is no-longer twice differentiable at all points, which is necessary in the proof of Theorem 2.4.4 and is an underlying issue in all jump conditions used. The proof then requires a different tactic that we will not discuss or have read. Lastly, when the geometries observe corners or cusps we can no-longer expect the density layer function smooth to any degree. As a consequence of the first problem, we can see that the jumps change at the corner points. Let \(x_j\) be the corners of the boundary, then

\[u_{\pm}(x) = \begin{cases} \pm\cfrac{\gamma^\pm_j}{2\pi}\tau(x_j) + [\mathcal{D}\tau](x_j) & x=x_j,\\ \pm\cfrac{1}{2}\tau(x) + [\mathcal{D}\tau](x) & x\neq x_j,\\ \end{cases}\]

with \(\gamma^+_j = \gamma_j\) and \(\gamma^-_j = 2\pi - \gamma_j\), and \(\gamma_j\) the interior angle at corner \(x_j\) in radians. The double layer potential can be reformulate to adapt to the corners

\[[\hat{\mathcal{D}}\tau](x) = \begin{cases} [\mathcal{D}\tau](x) + \left(\cfrac{\gamma_j}{\pi}-1\right)\tau(x), & x = x_j,\\ [\mathcal{D}\tau](x), & x\neq x_j. \end{cases}\]

Now here, for \(\tau\in C(\partial D)\), we have that \(\mathcal{D}\tau\) is not continuous at corners, but \(\hat{\mathcal{D}}\tau\) is. The existence of a solution is still true, however it is more intense to prove [8]. We now have that if the boundary data is \(L^2\), the density function \(\tau\in L^2(\partial D\). The limiting convergence at the boundary is now true is a weak sense, i.e.,

\[\lim_{h\to^+0}\int_{\partial D}\left(u(y+h\vec n(y))-f(y)\right)^2\mathrm{d}s(y) = 0.\]

2.5 The Laplacian's spectrum

The spectrum of the Laplacian is closely related to the Helmholtz equation and plays a vital role in both its uniqueness and existence, through BIE. We first introduce the problem statements an review all characteristics of the Laplacian's spectrum needed for the following chapter. We are particularly interested in the spectrum of the Laplacian with three boundary conditions: the Dirichlet, Neumann and Impedance (or Robin) boundary conditions.

Problem 2.5.1.

Let \(\Omega\) be a domain, find the eigenvalues \(\lambda\in\C\) and non-zero eigenfunctions \(u:D\to\mathbb{C}\) such that:

\[\begin{align*} -\Delta u(x) &= \lambda u(x)& \qquad x&\in D,\\ u(x) &= 0&\qquad x&\in\partial \Omega. \end{align*}\]

Problem 2.5.2.

Let \(\Omega\) be a domain, find the eigenvalues \(\lambda\in\C\) and non-zero eigenfunctions \(u:D\to\mathbb{C}\) such that:

\[\begin{align*} -\Delta u(x) &= \lambda u(x)& \qquad x&\in \Omega,\\ \frac{\partial u}{\partial \vec n}(x) &= 0&\qquad x&\in\partial \Omega. \end{align*}\]

Problem 2.5.3.

Let \(\Omega\) be a domain, find the eigenvalues \(\lambda\in\C\) and non-zero eigenfunctions \(u:D\to\mathbb{C}\) such that:

\[\begin{align*} -\Delta u(x) &= \lambda u(x)& \qquad x&\in \Omega,\\ \frac{\partial u}{\partial \vec n}(x) + \alpha u(x) &= 0&\qquad x&\in\partial \Omega, \end{align*}\]

with non-zero impedance parameter \(\alpha\) representing local resistance.

While the eigenvalues and corresponding eigenfunction are very useful for solving Laplace BVPs, they play a vital role in the well-posedness of BIE reformulations of the Helmholtz equation. To this end, we inspect a limited amount of information on the locations and geometry of the eigenvalues for both interior and exterior domains.
The location of the spectrum of the Laplace equation is found through the following spectral theorem [6].

Theorem 2.5.4 (Spectral theorem for self-adjoint operators).

Let \(\mathcal{A}\) be a self-adjoint operator on a Hilbert space \(H\), i.e., \(\mathcal{A}=\mathcal{A}^*\), then \(\sigma(\mathcal{A})\subset\R\).

The Laplacian is indeed self-adjoint with all boundary conditions (with \(\alpha\in\R\)), are self-adjoint in \(L^2(\Omega)\). Symmetry of the operator is seen through Green's first theorem. Let \(f,g\in C^2(\Omega)\) satisfying the homogeneous Dirichlet or Neumann boundary condition,

\[\langle\Delta f,g\rangle = \int_{\Omega}\Delta f~ \overline{g}~\mathrm{d}\Omega = -\int_{\Omega}\nabla \overline{g} \cdot \nabla f~\mathrm{d}\Omega = \int_{\Omega}f\overline{\Delta g} ~\mathrm{d}\Omega = \langle f,\Delta g\rangle.\]

For the impedance boundary condition, let \(f,g\in C^2(\Omega)\) satisfy the impedance boundary condition with \(\alpha\in\R\), i.e, \(\Dn f = -\alpha f\) and \(\overline{g} = -\frac{1}{\alpha}\frac{\partial \overline{g}}{\partial \vec n}\)

\[\langle\Delta f,g\rangle = \int_{\Omega}\Delta f~ \overline{g}~\mathrm{d}\Omega = -\int_{\Omega}\nabla \overline{g} \cdot \nabla f~\mathrm{d}\Omega + \int_{\partial \Omega}\overline{ g} \Dn f~\mathrm{d}\Gamma = -\int_{\Omega}\nabla\overline{ g} \cdot \nabla f~\mathrm{d}\Omega + \int_{\partial \Omega}\frac{\partial \overline{ g}}{\partial \vec n}~ f~\mathrm{d}\Gamma = \int_{\Omega}f\overline{\Delta g} ~\mathrm{d}\Omega = \langle f,\Delta g\rangle.\]

Proving \(\Delta \pm i\) is surjective to complete the self-adjoint-ness proof is outside the scope of class [6]. The spectrum is therefore real and we can even say something about its sign. For the Dirichlet and Neumann problem, if we multiply \(-\Delta u = \lambda u\) by \(\overline{u}\) and integrate over \(\Omega\), using Green's first theorem, we see that

\[\lambda \int_{\Omega}|u|^2~\mathrm{d}\Omega = \int_{\Omega}|\nabla u|^ 2\mathrm{d}\Omega.\]

Since both integral are positive, to have a non-trivial solution, we must have that \(\lambda>0\). Similarly for the impedance problem, we have

\[\lambda \int_{\Omega}|u|^2~\mathrm{d}\Omega = \int_{\Omega}|\nabla u|^2~\mathrm{d}\Omega - \int_{\partial \Omega}\overline{u}\frac{\partial u}{\partial \vec n}\mathrm{d}\Gamma = \int_{\Omega}|\nabla u|^2~\mathrm{d}\Omega + \alpha\int_{\partial \Omega}|u|^2\mathrm{d}\Gamma.\]

If \(\alpha\) is real and positive, the integrals and the right hand side are positive. In order to have a non-trivial eigenfunction we again must have that \(\lambda>0\).
We are also able to state if the spectrum is discrete, continuous or a mix, through theory on compact resolvents.

Definition 2.5.5 (Compact Resolvent).

A closed, densely defined operator \(\mathcal{A}\) on a Hilbert space \(H\) has compact resolvent if for some (equivalently, by the resolvent identity, every) \(\lambda\in\rho(\mathcal{A})\), the resolvent operator \((\mathcal{A}-\lambda I)^{-1}:H\to H \) is compact.

In particular, the Riesz–Schauder theorem [6, 8] states that if an operators resolvent is compact, it has a discrete spectrum.

Theorem 2.5.6 (Riesz–Schauder theorem).

If \(\mathcal{K}\) is a compact operator on a Hilbert space \(H\), then \(\sigma(\mathcal{K})\backslash \{0\}\) consists of isolated eigenvalues of finite algebraic multiplicity, with no other spectrum (continuous or residual) away from \(0\), and \(0\) is the only possible accumulations point.

The proof of the theorem and the fact that \(\Delta\), the Laplacian with considered boundary conditions, is closed is outside the scope of this report. If we use Riesz–Schauder theorem on \(\mathcal{K} = (\Delta - \lambda_0)^{-1}\), with \(\lambda_0\in\rho(\Delta)\), it can be shown that \(\sigma(\Delta)\) is discrete with isolated eigenvalues of finite algebraic multiplicity, accumulating only at \(\infty\). The Laplacian with given boundary conditions has a compact resolvent when the domain \(\Omega\) is has a compact resolvent. This is conceptually reasoned: on a bounded domain \(\Omega\), compactness of the resolvent is essentially automatic for any elliptic operator with a reasonable domain geometry. The resolvent behaves like a bounded solution operator into \(H^1(\Omega)\) composed with the inclusion \(H^1(\Omega) \hookrightarrow L^2(\Omega)\), and this inclusion is compact precisely because \(\Omega\) is bounded. This has been shown through the Rellich-Kondrachov theorem and fails on unbounded domains [4, 6]. Intuitively, a bounded \(H^1\) sequence has its gradient bounded and lives in a fixed finite region, so it cannot escape or oscillate its way out of precompactness in \(L^2\). However, on an unbounded domain, this compactness fails. A bounded sequence in \(H^1(\mathbb{R}^n)\) can be a sequence of translations of a fixed bump functions shifted off to infinity, which is bounded in \(H^1\) but admits no convergent subsequence in \(L^2(\mathbb{R}^n)\). As a result, on unbounded domains the Laplacian (with any boundary condition) typically has some continuous spectrum. Here, \(\sigma(-\Delta) = [0,\infty)\) on \(\Omega \subset \mathbb{R}^d\). This leads to the following two observations.

Observation 2.5.7.

The Laplacian with Dirichlet, Neumann or Impedance, with real impedance parameter, boundary conditions on the interior domain have real discrete spectrum only accumulating at infinity.

Observation 2.5.8.

The Laplacian with Dirichlet, Neumann or Impedance, with real impedance parameter, boundary conditions on the exterior domain have real continuous spectrum.

Lastly, we further discuss the impedance problem with a purely imaginary impedance parameter.

Problem 2.5.9.

Let \(\Omega\) be a domain, find the eigenvalues \(\lambda\in\mathbb{C}\) and non-zero eigenfunctions \(u:\Omega\to\mathbb{C}\) such that:

\[\begin{align*} -\Delta u(x) &= \lambda u(x) & x&\in \Omega,\\ \partial_n u(x) - i\eta u(x) &= 0 & x&\in\partial \Omega, \end{align*}\]

with real non-zero impedance parameter \(\eta\) representing local resistance.

It can be shown that this problems again has a compact resolvent for the associated operator, exactly as in the real-\(\alpha\) case [4], so by the Riesz–Schauder theorem [6] the spectrum \(\sigma(A)\) remains discrete. However, the symmetry of the operator does not hold, it is not self-adjoint and thus the eigenvalues are no-longer real valued. The location of the eigenvalues can still be found and it depends on the sign of \(\eta\). Multiply \(-\Delta u = \lambda u\) by \(\overline{u}\), integrate over the domain \(\Omega\) and apply Green's identity with the impedance boundary condition,

\[\lambda \int_{\Omega}|u|^2~\mathrm{d}\Omega = \int_{\Omega}|\nabla u|^2~\mathrm{d}\Omega - \int_{\partial \Omega}\overline{u}\frac{\partial u}{\partial \vec n}\mathrm{d}\Gamma = \int_{\Omega}|\nabla u|^2~\mathrm{d}\Omega - i\eta\int_{\partial \Omega}|u|^2\mathrm{d}\Gamma.\]

Let \(\lambda = \lambda_r + i\lambda_i\) with \(\lambda_r,\lambda_i\in\R\). Since all integral are real valued, taking the real part of both side tells us

\[\lambda_r\int_{\Omega}|u|^2~\mathrm{d}\Omega = \int_{\Omega}|\nabla u|^2~\mathrm{d}\Omega, \tag{2.20}\]

since both integral are positive, in order to obtain a non-trivial eigenfunction, we must have that \(\lambda_r\geq0\). Moreover, strict inequality holds \(\lambda_r>0\), if \(\lambda_r=0\), \(\nabla u = 0\), i.e., \(u\) would have to be constant. In fact, the boundary condition would be \(u=0\), hence \(u\equiv 0\) in the domain and thus \(u\) would not be an eigenfunction. Taking the imaginary part we see that

\[\lambda_i \int_{\Omega}|u|^2~\mathrm{d}\Omega = -\eta\int_{\partial \Omega}|u|^2\mathrm{d}\Gamma. \tag{2.21}\]

Since both integrals are positive, in order to have a non-trivial eigenfunction, we must have that \(\lambda_i\) and \(\eta\) have the opposite sign, i.e., if the \(\eta\) is negative, the eigenvalues will be in the upper-half-plane and if \(\eta\) is positive, the eigenvalues will be in the lower-half-plane. Note that \(\lambda_i\) cannot be real as then the eigenfunction would again be forced to be trivial. We thus have the concluding observation.

Observation 2.5.10.

The Laplacian with Impedance boundary condition with impedance parameter \(i\eta\) has a discrete spectrum in the upper-half-plane when \(\eta<0\) and lower-half-plane when \(\eta>0\).

References

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