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WAVES AND VIBRATIONS IN INHOMOGENEOUS STRUCTURES ...

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2.3 Experimental demonstration 11<br />

Figure 2.4 Experimental setup and part of the setup showing (from left to right) the<br />

vibration exciter, force transducer, periodic bar system with supporting threads, and<br />

accelerometer. From paper [2].<br />

[dB/1.00 (m/s†)/N]<br />

80<br />

60<br />

40<br />

20<br />

0<br />

-20<br />

FRF (Magnitude)<br />

Working : PMMA-Alu-11-seg-7.5cm-200302-ref : Input : FFT Analyzer<br />

-30<br />

a)<br />

0 2k 4k 6k 8k 10k 12k 14k<br />

[Hz]<br />

16k 18k 20k 22k 24k 26k<br />

b)<br />

0 2000 4000 6000 8000 10000 12000 14000 16000 18000 20000 22000 24000<br />

Hz<br />

dB<br />

Figure2.5 Responsecurvesshowingtheacceleration responseattheendofthebarversus<br />

the excitation frequency. Left: experimental data and right: corresponding theoretical<br />

predictions. From paper [2].<br />

2.3 Experimental demonstration<br />

The theoretical predictions are based on simple mass-spring models. Thus, it is<br />

here especially important to support observations and conclusions experimentally.<br />

In this way it can be documented that the bandgap phenomenon manifests itself in<br />

a realistic setup and is not merely the product of an overly simplified model.<br />

Fig. 2.4 illustrates a schematic and experimental setup for measuring the forced<br />

vibration response of an elastic rod composed of alternating sections of aluminum<br />

and PMMA (a plastic material). The rod is subjected to periodic forcing imposed<br />

by a shaker in one end and the acceleration is recorded in the other end using<br />

an accelerometer. Fig. 2.5 shows plots of the measured response and the response<br />

predicted by a mass-spring model fitted to the actual material parameters including<br />

a single fitted viscous damping parameter.<br />

80<br />

70<br />

60<br />

50<br />

40<br />

30<br />

20<br />

10<br />

0<br />

-10<br />

-20

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