30.07.2013 Views

WAVES AND VIBRATIONS IN INHOMOGENEOUS STRUCTURES ...

WAVES AND VIBRATIONS IN INHOMOGENEOUS STRUCTURES ...

WAVES AND VIBRATIONS IN INHOMOGENEOUS STRUCTURES ...

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

Inverse design of phononic crystals by tobology optimization 899<br />

PMMA<br />

f [kHz]<br />

band gap is smaller than the corresponding first (optimized)<br />

relative band gap for the single longitudinal case, while the<br />

second and third are actually larger. Also, the third relative<br />

band gap for bending waves is smaller (but not much) than<br />

the corresponding third (optimized) relative band gap for the<br />

single bending case. The similarity between this design and<br />

the bending case design (they are almost eachother’s mirrors)<br />

is also reflected in their performances, which are very close<br />

(relative band gaps of 0.374 and 0.378).<br />

Torsion waves in a beam are described by the same<br />

differential equation as for longitudinal waves, but with<br />

E K<br />

the factor<br />

replacing E. Here I is the area mo-<br />

2ð1 þ nÞ I<br />

ment of inertia as before and K is the torsion stiffness<br />

cross-sectional factor. For a circular cross-section K ¼ I<br />

and it may be seen that the torsional frequencies are lower<br />

than<br />

pffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi<br />

the longitudinal frequencies by a factor of<br />

2ð1 þ nÞ 1:6. Comparing the torsional frequency<br />

bands with the bands in Fig. 3 for the optimized design in<br />

the combined case shows that there is a band gap between<br />

10.6–13.2 kHz (relative band gap 0.43) for all three wave<br />

types, i.e. in this interval all three wave types are prevented<br />

from propagating in the beam.<br />

Since for all geometries K<br />

1 (with “¼” only for cir-<br />

I<br />

cular cross-sections), it is not possible to obtain<br />

K<br />

I<br />

Alu<br />

80<br />

60<br />

40<br />

20<br />

1 2 3 4 5 6 7 8<br />

[cm]<br />

0<br />

0 0.5 1 1.5<br />

k<br />

B<br />

2 2.5 3<br />

Fig. 3. Final design corresponding to maximum relative band gap between<br />

first and second band for longitudinal waves and third and<br />

fourth band for bending waves. Full lines: Longitudinal waves.<br />

Dashed lines: Bending waves.<br />

Table 4. Extreme frequency band values for bending and longitudinal<br />

waves in Fig. 3. Unit is kHz.<br />

B waves L waves<br />

k B ¼ 0 k B ¼ p k B ¼ 0 k B ¼ p<br />

f1 0 1.145 0 10.643<br />

f2 5.6165 1.6585 27.272 21.993<br />

f3 5.9774 10.643 42.172 45.188<br />

f4 21.454 15.534 77.451 72.706<br />

¼ 2ð1 þ nÞ which would result in perfectly coinciding<br />

[dB/1.00 (m/s†)/N]<br />

dB<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 />

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

[Hz]<br />

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

80<br />

70<br />

60<br />

50<br />

40<br />

30<br />

20<br />

10<br />

0<br />

-10<br />

-20<br />

-30<br />

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

Hz<br />

Fig. 4. Frequency response curves from [13]. Top: Experimental. Bottom:<br />

Theoretical.<br />

Table 5. Frequency band gaps in Fig. 4 determined by inspection.<br />

Unit is kHz.<br />

f min<br />

1<br />

f max<br />

1<br />

f min<br />

2<br />

f max<br />

2<br />

5.1 13.1 15.4 24.3<br />

torsional and longitudinal bands. To increase the common<br />

gap size, one may consider lowering the mid-gap values<br />

between higher torsional modes. This can be obtained by<br />

decreasing the ratio K<br />

which can be achieved by choosing<br />

I<br />

a non-circular cross-section. This aspect will be investigated<br />

in future work.<br />

In the following, the above results are compared with<br />

the experimental results presented in [13]. Here, the set-up<br />

is a (non-optimized) bar made up of five-and-a-half repetitions<br />

of a base section consisting of two bars glued together<br />

with circular cross-sections with diameter 1 cm and<br />

made of PMMA and Aluminum respectively, as in the<br />

above case. Each bar is 7.5 cm resulting in a base cell<br />

with a length of 15 cm. An experimental response curve<br />

showing the acceleration response at the end of the bar as<br />

a function of the longitudinal vibration excitation frequency<br />

applied to the opposite end is shown in Fig. 4<br />

(upper) with a corresponding theoretical prediction shown<br />

below. The 40 dB horizontal line has been used to identify

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!