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WAVES AND VIBRATIONS IN INHOMOGENEOUS STRUCTURES ...

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paper extends on this work. For an outline of the general method as well as examples<br />

of various applications see e.g. [5].<br />

We start out by describing the governing equation and discuss the basic material<br />

interpolation scheme on the basis of a simple acoustic model. We solve the model equations<br />

using a FEM procedure, and move on to illustrating the optimization algorithm<br />

for a sample problem. Lastly, we give conclusion and directions for further work.<br />

ACOUSTIC MODEL<br />

We consider a plane model of steady-state acoustic wave propagation, modelled by the<br />

2D Helmholtz equation:<br />

∇ · (ρ −1 ∇p) + ω 2 κ −1 p = 0. (1)<br />

In Eq. (1), p is a complex pressure amplitude, ρ and κ are the position dependent density<br />

and bulk modulus of the acoustic medium. The wave frequency is denoted ω.<br />

The optimization problem is to distribute two materials (air and solid), in a design<br />

domain Ωd, so that some functional Φ(ω,ρ,κ, ∇p,p) is extremized. The two materials<br />

have the following set of material properties: (ρ,κ) = (ρ1,κ1) (air), and (ρ,κ) =<br />

(ρ2,κ2) (solid). It should be emphasized that the present pure-acoustic model neglects<br />

any acoustic-structure interaction. For large values of ρ2κ2 the solid is practically a<br />

perfectly rigid and thus fully reflecting, whereas for smaller values it represents an<br />

acoustic medium.<br />

We rescale the equations by introducing the new variables:<br />

<br />

1, air<br />

1, air<br />

˜ρ = ρ<br />

ρ1<br />

=<br />

and inserting them into Eq. (1):<br />

ρ2<br />

ρ1<br />

, solid , ˜κ = κ<br />

κ1<br />

=<br />

κ2,<br />

solid κ1<br />

(2)<br />

∇ · (˜ρ −1 ∇p) + ˜ω 2 ˜κ −1 p = 0, (3)<br />

where ˜ω = ω/c is a scaled wave frequency and c = κ1/ρ1 is the speed of sound in<br />

air. In the following the tildes will be omitted for simplicity.<br />

We may apply different boundary conditions to simulate incoming waves, as well<br />

as reflecting and absorbing boundaries. Additionally, perfectly matching layers can be<br />

added to the model such that low reflection at radiating boundaries is ensured for all<br />

angles of incidence.<br />

DESIGN VARIABLES <strong>AND</strong> MATERIAL <strong>IN</strong>TERPOLATION<br />

The basis of the topology optimization method is to let the "material" properties ρ and κ<br />

take not only the discrete values of air and solid (cf. Eq. (2)), but also any intermediate<br />

values. To facilitate this, we introduce a continuous material indicator field 0 ≤ ̺ ≤ 1,<br />

2

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