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WAVES AND VIBRATIONS IN INHOMOGENEOUS STRUCTURES ...

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896 S. Halkjær, O. Sigmund and J. S. Jensen<br />

distributions. The design variables are spatial material densities.<br />

By using analytical sensitivity analysis and mathematical<br />

programming tools it is possible efficiently to handle<br />

a large number of design variables. We base our<br />

implementation on Finite Element (FE) modelling and typically<br />

choose one continuous design variable per element<br />

or node:<br />

z e 2 R ; e ¼ 1; ...; N ; ð1Þ<br />

where N is the number of finite elements or nodes in the<br />

design domain. It should be emphasized that the method<br />

can be used with a finite difference discretization just as<br />

easily and that more design variables can be assigned to<br />

each element in order to distribute more than two materials<br />

in the design domain.<br />

The goal for the optimization algorithm is to distribute<br />

two materials in a domain such that some cost function is<br />

minimized (or maximized). The continuous design variables<br />

control the material distribution by defining the element-wise<br />

constant material properties in each element. If<br />

r e denotes an element-wise property we can write:<br />

r e ¼ð1 z eÞ r 1 þ r 2 z e ð2Þ<br />

where subscript 1 and 2 refers to the properties of material<br />

1 and material 2, respectively. In this case we let z e vary<br />

continuously between 0 and 1, such that for z e ¼ 0 the<br />

corresponding element takes the material properties of material<br />

1 and for z e ¼ 1 those of material 2.<br />

Denoting the cost function F we can now formulate<br />

the optimization problem as follows:<br />

min:<br />

F ¼ Fðw; u; zÞ ; ð3Þ<br />

z<br />

s:t:: giðzÞ g* i ; ð4Þ<br />

0 ze 1 ; e ¼ 1; ...; N ; ð5Þ<br />

ðK w 2 MÞ u ¼ f ; ð6Þ<br />

where Eq. (6) is the discretized FE equation of the timeharmonic<br />

wave propagation problem. The vector u contains<br />

the discretized nodal values of the complex amplitudes<br />

of the displacement field, and K and M are the stiffness<br />

and mass matrices, respectively. The load vector f<br />

comes from external wave loading. In (4) a number of<br />

additional constraints can be specified, e.g. specifying a<br />

maximum amount of a single material component. For<br />

more details about computational procedures, sensitivity<br />

analysis and more, the reader is referred to [2].<br />

The advantage of using continuous design variables is<br />

that it allows for the use of efficient gradient-based optimization<br />

algorithms. However, it also implies that we may<br />

end up with values of z e that are neither 0 or 1, but an<br />

intermediate value that does not correspond to any of the<br />

two materials. There are several ways to penalize the appearance<br />

of intermediate density solutions (see e.g. [2]),<br />

however, it is our experience that intermediate densities<br />

seldomly remain in the optimized band gap designs since<br />

band gaps are favoured by maximum contrast in the material<br />

properties. Therefore we have not used any penalization<br />

techniques in this work.<br />

As for all topology optimization problems with spatial<br />

material distribution the results depend on the mesh. How-<br />

ever, as opposed to conventional stiffness design problems<br />

where the objective is improved with mesh-refinement, it<br />

appears that the finite length of the elastic waves imposes<br />

a length-scale for the present band gap design problems<br />

and thus we do usually not experience a significant meshdependence.<br />

Therefore, we do not use regularization techniques<br />

in this paper. For more discussions of this issue,<br />

the reader is referred to [2]. Concerning the convergence<br />

of the finite element model, we require discretizations that<br />

at least have 10 elements pr. wave-length. Due to the reasons<br />

discussed above, we do not expect to find significantly<br />

different design solutions if the mesh is further refined.<br />

Design of 1D structures:<br />

the infinite periodic elastic beam<br />

In this section, we study elastic wave propagation in a<br />

periodic beam of infinite length. The beam consists of an<br />

infinite number of copies of a base cell with a specific<br />

geometry and material distribution. The periodicity introduces<br />

frequency band gaps for both longitudinal and bending<br />

waves, preventing waves with frequencies in these<br />

gaps from propagating in the beam. In general, the band<br />

gap frequency ranges for the two wave types are different,<br />

but for certain geometries and material distributions of the<br />

base cell, band gaps for the two wave types overlap, preventing<br />

both of the two wave types from propagating in<br />

the beam. Such studies are relevant in design problems<br />

where vibration insulation and filtering are important objectives.<br />

Theory<br />

Let the beam axis be directed along the x-axis. Longitudinal<br />

wave propagation in the beam is described using the<br />

usual 1D theory<br />

@<br />

@x<br />

@u<br />

E<br />

@x ¼ q @2u @t2 ð7Þ<br />

where u ¼ uðx; tÞ denotes the displacement along the x-axis.<br />

q denotes the mass density and E is Young’s modulus.<br />

Bending waves in the beam are described by Timoshenko<br />

theory<br />

@<br />

@x<br />

@<br />

@x<br />

ksGA @w<br />

@x þ q ¼ qA @2w ; ð8Þ<br />

@t2 EI @q<br />

@x<br />

ksGA @w<br />

@x þ q ¼ qI @2q @t2 ð9Þ<br />

where w ¼ wðx; tÞ and q ¼ qðx; tÞ denote the transverse<br />

displacement and angle of rotation of the cross-section respectively.<br />

A, I, G and ks denote the cross-sectional area,<br />

area moment of inertia, shear modulus and the shear correction<br />

coefficient, respectively. Here, we use<br />

ks ¼ 6ð1 þ nÞ=ð7 þ 6nÞ [14] for a circular cross-section,<br />

where n is the Poisson ratio. Timoshenko theory is used,<br />

as the ratio between considered wave length and cross-section<br />

dimension is smaller than the lower bound ( 20) for<br />

using the simpler Bernoulli-Euler theory.

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