Abstract
The matrix characterizing nonuniqueness of solution for Fredholm integral equations of the first kind is constructed and approximated numerically in the case of plane elastic deformations.
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10.1 Introduction
Let S be a finite domain in \(\mathbb{R}^{2}\), bounded by a simple, closed, C 2 curve \(\partial S\). We denote by x and y generic points in \(S \cup \partial S\) and by | x − y | the distance between x and y in the Cartesian metric. Also, let C 0, α(∂ S) and C 1, α(∂ S), α ∈ (0, 1), be, respectively, the spaces of Hölder continuous and Hölder continuously differentiable functions on \(\partial S\). In what follows, Greek and Latin indices take the values 1, 2 and 1, 2, 3, respectively, and a superscript T denotes matrix transposition.
For any function f continuous on \(\partial S\), we define the ‘calibration’ functional p by
Using the fundamental solution for the two-dimensional Laplacian
we define the single-layer harmonic potential of density φ by
The proof of the following assertion can be found, for example, in [Co94] or [Co00].
Theorem 1.
For any α ∈ (0,1), there are a unique nonzero function Φ ∈ C 0,α (∂S) and a unique number ω such that
It is easy to see that Φ and ω depend on g and ∂ S.
The numbers 2π ω and e −2π ω are called Robin’s constant and the logarithmic capacity of ∂ S.
For a circle with the center at the origin and radius R, both Φ and ω can be determined explicitly:
For other boundary curves, Φ and ω are practically impossible to determine analytically and must be computed by numerical methods.
If the solution of the Dirichlet problem in S with data function f on ∂ S is sought as u = V φ, then φ is a solution of the (weakly singular) first-kind boundary integral equation
This is a well-posed problem if and only if ω ≠ 0. If ω = 0, the above equation has infinitely many solutions, which are expressed in terms of Φ.
10.2 Plane Elastic Strain
Consider a plate made of a homogeneous and isotropic material with Lamé constants λ and μ, which undergoes deformations in the (x 1, x 2)-plane. If the body forces are negligible, then its (static) displacement vector u = (u 1, u 2)T satisfies the equilibrium system of equations [Co00]
where
It is not difficult to show [Co00] that the columns F (i) of the matrix
form a basis for the space of rigid displacements.
The ‘calibrating’ vector-valued functional p is defined for continuous 2 × 1 vector functions f by
A matrix of fundamental solutions for A is [Co00]
The single-layer potential of density φ is defined by
The proof of the following assertion can be found in [Co00].
Theorem 2.
There is a unique 2 × 3 matrix function Φ ∈ C 0,α (∂S) and a unique 3 × 3 constant symmetric matrix \(\mathcal{C}\) such that the columns Φ (i) of Φ are linearly independent and
where I is the identity matrix.
Clearly, Φ and \(\mathcal{C}\) depend on A, D, and ∂ S.
In the so-called alternative indirect method [Co00], the solution of the Dirichlet problem in S with data function f on ∂ S is sought in the form
Then the problem reduces to the (weakly singular) boundary integral equation
Theorem 3.
Equation (10.2) has a unique solution φ ∈ C 0,α (∂S), α ∈ (0,1), for any f ∈ C 1,α (∂S) if and only if \(\det \mathcal{C}\not =0\) . In this case, (10.1) is the unique solution of the Dirichlet problem.
If \(\det \mathcal{C} = 0\), then the unique solution of the Dirichlet problem is obtained by solving an ill-posed modified boundary integral equation whose infinitely many solutions are constructed with Φ and \(\mathcal{C}\).
In the so-called refined indirect method [Co00], the solution of the Dirichlet problem is sought as a pair {φ, c} such that
where s a constant 3 × 1 vector chosen (arbitrarily) a priori and c is a constant 3 × 1 vector. This leads to the system of boundary integral equations
Theorem 4.
System (10.3) has a unique solution {φ, c} with φ ∈ C 0,α (∂S) for any f ∈ C 1,α (∂S), α ∈ (0,1), and any s.
It is important to evaluate the arbitrariness in the representation of the solution with respect to the prescribed ‘calibration’ s.
Theorem 5.
If {φ (1) , c (1) }, {φ (2) , c (2) } are two solutions of (10.3) constructed with s (1) and s (2) , respectively, then
It is not easy to compute Φ and \(\mathcal{C}\) analytically, or even numerically, in arbitrary domains S, but this can be accomplished if S is a circular disk. Let ∂ S be the circle with center at the origin and radius R. In this case, Φ and \(\mathcal{C}\) can be determined analytically as
Clearly, \(\det \mathcal{C} = 0\) if and only if \(R = e^{-1}\).
Analytic computation of Φ and \(\mathcal{C}\) is practically impossible for non-circular domains, and must be performed numerically.
We choose four 3 × 1 constant vectors s (0), s (i) such that the set {s (i) − s (0)} is linearly independent, and form the 3 × 3 matrix \(\varSigma\) with columns s (i) − s (0). Also, we choose an arbitrary function f. Next, we compute the solutions {φ (0), c (0)}, {φ (i), c (i)} of (10.3) corresponding to s (0), s (i), respectively, and f, by the refined indirect method, then form the 2 × 3 matrix function Ψ with columns φ (i) −φ (0) and the constant 3 × 3 matrix Γ with columns c (i) − c (0).
From Theorem 4 it follows that
or, what is the same,
hence,
A similar analysis can be performed for other two-dimensional linear elliptic systems with constant coefficients—for example, the system modeling bending of elastic plates with transverse shear deformation [Co00]. No apparent connection exists between the matrix \(\mathcal{C}\) and the characteristic constant ω of ∂ S.
10.3 Numerical Examples
Consider a steel plate with scaled Lamé coefficients
and let ∂ S (see Figure 10.1) be the curve of parametric equations
We choose the vectors
The approximating functions for computing φ (0)(t) and φ (i)(t) are piecewise cubic Hermite splines on 12 knots; that is, the interval 0 ≤ t ≤ 2 is divided into 12 equal subintervals. Then the characteristic matrix (with entries rounded off to 5 decimal places) is
Here,
The graphs of the components Φ α i of Φ are shown in Figure 10.2.
As a second example, consider the ‘expanding’ ellipse ∂ S of parametric equations
The graph of \(\det \mathcal{C}\) as a function of k is shown in Figure 10.3.
Here, \(\det \mathcal{C} = 0\) for k = 0. 22546 and k = 0. 26934.
References
Constanda, C.: On integral solutions of the equations of thin plates. Proc. Roy. Soc. London Ser. A, 444, 261–268 (1994).
Constanda, C.: Direct and Indirect Boundary Integral Equation Methods, Chapman & Hall/CRC, Boca Raton, FL (2000).
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Constanda, C., Doty, D.R. (2015). The Characteristic Matrix of Nonuniqueness for First-Kind Equations. In: Constanda, C., Kirsch, A. (eds) Integral Methods in Science and Engineering. Birkhäuser, Cham. https://doi.org/10.1007/978-3-319-16727-5_10
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DOI: https://doi.org/10.1007/978-3-319-16727-5_10
Publisher Name: Birkhäuser, Cham
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