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Oscillations, Waves, and Interactions - GWDG

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(pressure drop) / (dynamic pressure)<br />

0.32<br />

0.3<br />

0.28<br />

0.26<br />

0.24<br />

0.22<br />

0.2<br />

0.18<br />

0.16<br />

0.14<br />

Sound absorption, sound amplification, <strong>and</strong> flow control in ducts 83<br />

(a)<br />

0.12<br />

0.12 0.14 0.16 0.18 0.2 0.22 0.24<br />

(b)<br />

0.12 0.14 0.16 0.18 0.2 0.22 0.24 0.26 0.28<br />

argument of function DP in Eq. (1)<br />

Figure 9. Relation between the pressure drop <strong>and</strong> the pressure amplitude at the rear end<br />

of the resonator section according to Eq. (1). (a) m = 0; pac = transmitted sound pressure<br />

amplitude; U/c = 0.2 (thin curves), frequencies: 907 Hz (black, dash-dotted), 1007 Hz (red,<br />

solid), 1087 Hz (green, dashed); U/c = 0.25 (thick curves), frequencies: 1007 Hz (black,<br />

dash-dotted), 1087 Hz (red, solid), 1127 Hz (green, dashed). (b) m = 1, pac = pressure<br />

amplitude in the backmost cavity; U/c = 0.2 (thin curves), frequencies: 1207 Hz (red,<br />

solid), 1307 Hz (green, dashed); U/c = 0.25 (thick curve), frequency: 1207 Hz (red, solid).<br />

(iv) The pressure drop ∆p along the lined duct section <strong>and</strong> the amplitude pac of the<br />

transmitted sound wave are related by<br />

�� �2 � �2<br />

∆p<br />

ptb κ(f, U) · pac<br />

= DP (U) +<br />

pdyn pdyn<br />

pdyn<br />

�<br />

, (1)<br />

wherein pdyn is the dynamic pressure. The quantities ptb(U) <strong>and</strong> κ(f, U) are fitted<br />

to the experimental data except for a free common factor which is adapted such<br />

that DP{· · ·} becomes the identity function for small sound pressure amplitudes;<br />

κ(f, U) increases with increasing frequency <strong>and</strong> with decreasing flow velocity. As<br />

seen from Fig. 9(a), DP{· · ·} does not differ very much from the identity function<br />

also at large sound amplitudes. However, only a few experimental data were suited<br />

for this evaluation, so the universality of DP{· · ·} may be questioned. In fact, when<br />

higher-order mode sound irradiation (see next Section) is applied to the resonator<br />

section, strongly nonlinear <strong>and</strong> all but universal relations are found between ∆p <strong>and</strong><br />

p 2 ac. Fig. 9(b) shows several examples where pac is the pressure amplitude in the<br />

backmost cavity of the resonator section.

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