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Oscillations, Waves, and Interactions - GWDG

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76 D. Ronneberger et al.<br />

(flow velocity) / (speed of sound) power spectral density<br />

40<br />

db<br />

20<br />

10<br />

0<br />

0.3<br />

0.2<br />

0.3<br />

0.2<br />

0.1<br />

a<br />

b<br />

A 1<br />

A 1<br />

0.1<br />

0 10 20 30 dB 40<br />

c<br />

1 A<br />

0 1 2<br />

frequency [kHz]<br />

3 4<br />

Figure 2. Power spectral density (psd) of the pressure downstream <strong>and</strong> upstream of the<br />

resonator section: (a) U/c = 0.27, downstream; (b) difference to the median of the distribution<br />

of the psd, as a function of the flow velocity, downstream; (c) same as (b), but<br />

upstream.<br />

dependence on the incident sound amplitude [25–28]. These phenomena have meanwhile<br />

turned out to be the effect of a strong seemingly convective instability of the<br />

turbulent flow in the lined duct section. Various experimental observations <strong>and</strong> some<br />

qualitative explanations of the phenomena will be presented in Sects. 2 <strong>and</strong> 3 while<br />

the attempts <strong>and</strong> the difficulties to underst<strong>and</strong> the instability will be discussed in<br />

Sect. 4.<br />

2 Experimental observations<br />

2.1 Axisymmetric mode<br />

2.1.1 Turbulent pressure fluctuations, sound transmission <strong>and</strong> static pressure drop<br />

The sound amplification <strong>and</strong> the acoustic influence on the static pressure occur at<br />

frequencies slightly above the first radial resonance frequency of the cavities. In<br />

contrast to the original study with frequencies well below the resonance frequency,<br />

most of the experiments to be reviewed in the following have therefore been performed<br />

A 2<br />

A 2<br />

2 A<br />

D<br />

B1<br />

A 3

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