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WAVES AND VIBRATIONS IN INHOMOGENEOUS STRUCTURES ...

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eplacemen<br />

22 Chapter 3 Bandgap structures as optimal designs<br />

Reflectance<br />

a) b)<br />

Reflectance<br />

c) d)<br />

1.0<br />

0.8<br />

0.6<br />

0.4<br />

0.2<br />

0.0<br />

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1.0<br />

0.8<br />

0.6<br />

0.4<br />

0.2<br />

Frequency (Hz)<br />

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Frequency (Hz)<br />

Figure 3.4 Optimized distribution of scattering (black) and host material (white) for<br />

maximum reflectance in a frequency interval around 788Hz and reflectance curves for the<br />

optimized designs for pressure (solid line) and shear waves (dashed line). a,b) ±10%<br />

frequency interval, c,d) ±25% frequency interval. From paper [6].<br />

are given for a pressure wave (a), a shear wave (b) and for both a shear and a<br />

pressure wave (c). The appearance of the structures reflects the multi-angle wave<br />

incidence that provokes the two-dimensional nature of the material distribution.<br />

The restricted spatial dimension also gives the structures appearances that are not<br />

regularly periodic.<br />

The results show that adding a third material to the design problem has no<br />

beneficial effect on reducing the transmission of waves. In all reported cases the best<br />

performance is obtained for a structure that is composed of the two materials having<br />

the largest contrast between their material properties. For a further discussion of<br />

this observation see the comments in the last paragraph of this chapter.<br />

3.3 Eigenfrequency separation<br />

The optimized structures strongly depend on the specific location of the input force<br />

and/or the direction of the incoming wave. Hence, a unidirectional wave usually<br />

results in a one-dimensional structure (Bragg grating) optimized for exactly this<br />

form of excitation. Other excitation types as in the form of multi-directional waves<br />

result in different structures. If the structure is to be optimized for all relevant<br />

loading conditions, the problem of how to specify these loading conditions arises.<br />

An alternative to this approach is to consider the structural eigenfrequencies. If<br />

frequency ranges with no eigenfrequencies can be created, then no loading condition

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