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Introduction to Acoustics

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94 Part A Propagation of Sound<br />

Part A 3.16<br />

consists of a cavity of volume V with a neck of length ℓ<br />

and cross-sectional area A.<br />

In the limit where the acoustic frequency is sufficiently<br />

low that the wavelength is much larger than any<br />

dimension of the resona<strong>to</strong>r, the compressible fluid in the<br />

resona<strong>to</strong>r acts as a spring with spring constant<br />

ksp = ρc2 A2 , (3.599)<br />

V<br />

and the fluid in the neck behaves as a lumped mass of<br />

magnitude<br />

m = ρAℓ ′ . (3.600)<br />

Here ℓ ′ is ℓ plus the end corrections for the two ends of<br />

the neck. If ℓ is somewhat larger than the neck radius a,<br />

and if both ends are terminated by a flange, then the two<br />

end corrections are each 0.82a. (The determination of<br />

end corrections has an extensive his<strong>to</strong>ry; a discussion can<br />

be found in the text by the author [3.30].) The resonance<br />

frequency ωr, in radians per second, of the resona<strong>to</strong>r is<br />

given by<br />

where<br />

ωr = 2π fr = (ksp/m) 1/2 = (MACA) −1/2 , (3.601)<br />

MA = ρℓ ′ /S (3.602)<br />

gives the acoustic inertance of the neck and<br />

CA = V/ρc 2<br />

(3.603)<br />

gives the acoustic compliance of the cavity. The ratio of<br />

the complex pressure amplitude just outside the mouth<br />

of the neck <strong>to</strong> the complex volume velocity amplitude<br />

of flow in<strong>to</strong> the neck is the acoustic impedance ZHR of<br />

the Helmholtz resona<strong>to</strong>r and given, with the neglect of<br />

damping, by<br />

ZHR =−iωMA +<br />

1<br />

, (3.604)<br />

−iωCA<br />

which vanishes at the resonance frequency.<br />

If a Helmholtz resona<strong>to</strong>r is inserted as a side branch<br />

in<strong>to</strong> the wall of a duct, it acts as a reactive muffler that<br />

has a high insertion loss near the resonance frequency<br />

of the resona<strong>to</strong>r. The analysis assumes that the acoustic<br />

3.16 Ray <strong>Acoustics</strong><br />

When the medium is slowly varying over distances comparable<br />

<strong>to</strong> a wavelength and if the propagation distances<br />

U(0 – )<br />

UHR<br />

p(0 – ) = p(0 + )<br />

U(0 + )<br />

Fig. 3.50 Helmholtz resona<strong>to</strong>r as a side-branch in a duct<br />

pressures in the duct just before and just after the resona<strong>to</strong>r<br />

are the same as the pressure at the mouth of the<br />

resona<strong>to</strong>r. Also, the acoustical analog of Kirchhoff’s circuit<br />

law for currents applies, so that the volume velocity<br />

flowing in the duct ahead of the resona<strong>to</strong>r equals the sum<br />

of the volume velocities flowing in<strong>to</strong> the resona<strong>to</strong>r and<br />

through the duct just after the resona<strong>to</strong>r. These relations,<br />

with (3.604), allow one <strong>to</strong> work out expressions for the<br />

amplitude reflection and transmission coefficients at the<br />

resona<strong>to</strong>r, the latter being given by<br />

2ZHR<br />

Ì =<br />

. (3.605)<br />

2ZHR + ρc/AD<br />

The fraction of incident power that is transmitted is<br />

consequently given by<br />

�<br />

1<br />

τ = 1 +<br />

4β2 ( f/ fr − fr/ f ) 2<br />

�−1 , (3.606)<br />

where β is determined by<br />

β 2 = (MA/CA)(AD/ρc) 3 . (3.607)<br />

The fraction transmitted is formally zero at the resonance<br />

frequency, but if β is large compared with unity, the<br />

bandwidth over which the drop in transmitted power is<br />

small is narrow compared with fr.<br />

are substantially greater than a wavelength, it is often<br />

convenient <strong>to</strong> regard acoustic fields as being carried<br />

x

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