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Oscillations, Waves, and Interactions - GWDG

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74 D. Ronneberger et al.<br />

Mechel found out that the sound attenuation in a channel the wall of which is<br />

equipped with periodically spaced Helmholtz resonators is considerably reduced in<br />

the presence of mean flow <strong>and</strong> may even be turned into sound amplification at certain<br />

frequencies [2]. The relation between these frequencies, the flow velocity <strong>and</strong><br />

the spacing of the resonators revealed a close analogy between the observed sound<br />

amplification <strong>and</strong> the amplification of electromagnetic waves in the so called travelling<br />

wave tube which exploits the interaction between the electromagnetic wave<br />

<strong>and</strong> an electron beam via a periodic structure [3]. However, the mechanism itself<br />

by which mean-flow energy is converted to sound energy remained unclear. Besides<br />

the sound amplification the excitation of loud tones was observed by Mechel when<br />

the resonators were undamped. The latter phenomenon is known also from isolated<br />

resonators the openings of which are exposed to grazing flow. A salient example of<br />

such self-excited pressure oscillations has occurred in a gas transport system where<br />

a pair of pipes with closed valves at the end branch off the main pipe in opposite<br />

directions. The pressure amplitudes were so large that the flow velocity had to be<br />

reduced in order to maintain safe operating conditions [4].<br />

The phenomena observed by Mechel are two examples of aero-acoustic instabilities<br />

which are based on the so called Kelvin-Helmholtz instability of vortex sheets. Such<br />

vortex sheets form at the interface between the Helmholtz resonators <strong>and</strong> the interior<br />

of the flow duct. While the sound amplification <strong>and</strong> the self-excited tones are closely<br />

related to the inhomogeneity of the channel, namely to the spacing of the resonators<br />

<strong>and</strong> maybe to the width of their openings, similar phenomena are also caused by<br />

homogeneous compliant walls that bound internal <strong>and</strong> external flows.<br />

The interest in the stability of fluid flow along compliant walls has been stimulated<br />

by the experiments which M. O. Kramer had performed to explain Gray’s paradox:<br />

Gray [5], wondering about the fast swimming speed of some dolphin species, had<br />

calculated that the dolphin’s muscles had to deliver a multiple of the mechanical<br />

power that is produced by the muscles of all other mammals unless the dolphins<br />

are able to control the flow in the boundary layer around their body to remain<br />

laminar. Kramer [6] speculated that the particular mechanical properties of the<br />

dolphin’s skin stabilize the flow, <strong>and</strong> in fact, with special compliant coatings of his test<br />

bodies he obtained an appreciable drag force reduction. However trials to reproduce<br />

these spectacular results in other laboratories have failed. The seminal theoretical<br />

investigation by Benjamin [7] <strong>and</strong> an impressive number of subsequent investigations<br />

some of which are still in progress have nevertheless shown that the compliance of the<br />

wall has indeed a strong effect on the stability of the flow boundary layer (see, e. g.,<br />

Refs. [8,9]). The flow is destabilized in most cases because of a whole zoo of instability<br />

modes that arise by the compliance of the wall, but under special circumstances a<br />

stabilization can be achieved, <strong>and</strong> there is little doubt meanwhile that the onset of<br />

turbulence can be delayed by appropriate coating of the wall.<br />

In connection with sound propagation in acoustically treated flow ducts the existence<br />

of the mentioned kind of instability has first been noted in theoretical studies<br />

[10–16], however, there was no indication that these modes really exist in the<br />

turbulent environment of practical flow situations. Nevertheless, the excitation of instability<br />

modes at the leading edge of the compliant wall was taken into account, <strong>and</strong><br />

it was assumed that the growing instability modes loose their coherence by nonlinear

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