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Oscillations, Waves, and Interactions - GWDG

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Sound absorption, sound amplification, <strong>and</strong> flow control in ducts 77<br />

peak frequency [kHz] peak amplitude [dB]<br />

50<br />

40<br />

30<br />

20<br />

10<br />

1<br />

0<br />

1.6<br />

1.4<br />

1.2<br />

gap width = 5 mm<br />

10<br />

6 cavities<br />

8<br />

5 mm 10 12.5<br />

10<br />

13 16<br />

0.15 0.2 0.25 0.3 0.35<br />

(flow velocity) / (speed of sound)<br />

6<br />

8<br />

13<br />

10 cavities<br />

Figure 3. Amplitude <strong>and</strong> mid-frequency of the A 1 -peak of Fig. 2(b) as functions of the flow<br />

velocity. The number of cavities has been varied while the full cross-section of the pipe was<br />

open to the flow (blue <strong>and</strong> black solid curves, denoted by the number of cavities), <strong>and</strong> the<br />

cross-section of the duct was reduced by insertion of a coaxial cylindrical body while the<br />

number of cavities (16) remained constant (red dashed curves, denoted by the gap width<br />

between the central body <strong>and</strong> the duct wall).<br />

with a low resonance frequency (840 Hz) corresponding to the dimensions of the<br />

cavities that are shown in Fig. 1. The lowest cut-on frequency of higher-order modes<br />

in the rigid pipes upstream <strong>and</strong> downstream of the resonator section is 4 kHz. So<br />

for frequencies in the order of the resonance frequency all higher-order modes are<br />

evanescent <strong>and</strong> only the fundamental axisymmetric mode can propagate.<br />

We first became aware of the sound amplification by some faint narrow-b<strong>and</strong> whispering<br />

superimposed on the flow noise in the laboratory. The pressure spectra (Fig. 2)<br />

measured far upstream <strong>and</strong> far downstream of the resonator section reveal that this<br />

sound originates in the resonator section <strong>and</strong> is radiated mainly in the direction of<br />

the flow. The sample spectrum in Fig. 2(a) shows a few prominent peaks on top of<br />

an otherwise rather constant power spectral density, <strong>and</strong> the development of these<br />

peaks with increasing flow velocity † U is depicted in Figs. 2(b) <strong>and</strong> (c) where the<br />

† Although the compressibility of the air is not essential for the considered phenomena,<br />

the average of the flow velocity over the cross-sectional area of the pipe U is normalized to<br />

12.5<br />

16

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