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Oscillations, Waves, and Interactions - GWDG

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Sound absorption, sound amplification, <strong>and</strong> flow control in ducts 85<br />

power spectral density<br />

coherence function<br />

10<br />

1<br />

.1<br />

1<br />

0.5<br />

0<br />

−0.5<br />

−1<br />

1<br />

0.5<br />

0<br />

a<br />

n=<br />

m=<br />

b<br />

0<br />

1<br />

0<br />

2<br />

1<br />

0<br />

0<br />

3<br />

0 1<br />

4 1<br />

0 1 2 0<br />

5 2 0 6<br />

1<br />

3<br />

2 0<br />

1 7<br />

−0.5<br />

c<br />

−1<br />

0 1 2 3 4 5<br />

frequency [kHz]<br />

Figure 11. Average of the data of Fig. 10 over 0.13 ≤ U/c ≤ 0.25. The cut-on frequencies<br />

of the various modes in the resonator section are marked on the bottom of Fig. (a) where<br />

the radial order of the modes are denoted by n, <strong>and</strong> the expected coherence functions (see<br />

text) are shown as dashed curves in Figs. (b) <strong>and</strong> (c).<br />

by a polynomial which was fitted to the logarithm of the power spectral density<br />

(psd), <strong>and</strong> only the difference between the actual psd <strong>and</strong> this ‘background spectrum’<br />

is presented as a function of the frequency <strong>and</strong> the flow velocity in figure 10a.<br />

As in Fig. 2(b) the peaks A 1 , A 2 , <strong>and</strong> A 3 are the the most outst<strong>and</strong>ing ones also in<br />

Fig. 10(a) where the fourth harmonic A 4 is included.<br />

In addition quite a few less prominent peaks appear in Fig. 10(a) which have no<br />

correspondence in Fig. 2(b). These peaks are therefore supposed to originate from<br />

higher-order modes which are evanescent in the rigid pipes. With one exception<br />

(C), the mid-frequencies of the additional peaks do not depend on the flow velocity.<br />

So the clearness of these peaks can be increased by averaging the spectra over a<br />

range U/c = 0.13 · · · 0.25 of flow velocities, within which the less prominent peaks<br />

more or less dominate over the A-peaks. The average is shown in Fig. 11(a), <strong>and</strong><br />

moreover the cut-on frequencies of the higher-order modes in the resonator section<br />

are marked on the frequency axis; the cut-on frequencies are only weakly dependent<br />

on the flow velocity <strong>and</strong> therefore have been computed for air at rest. A steep increase<br />

of the power spectral density is found at the low-order cut-on frequencies. So it is<br />

conjectured that the contribution to the pressure fluctuations by a definite mode is<br />

particularly large at frequencies just above the respective cut-on frequency.

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