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Introduction to Acoustics

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For travelling waves,ei(ωt±kx) , this results in a ratio between<br />

the pressure and flow rate, defined as the tube<br />

impedance<br />

Z = p<br />

U =±ρc0 , (15.94)<br />

S<br />

where the plus and minus signs refer <strong>to</strong> waves travelling<br />

in the positive and negative x-directions, respectively.<br />

There is a very close analogy with an electrical transmission<br />

line, with pressure and flow rate the analogue<br />

of voltage and current, as discussed later. Because the<br />

impedance is inversely proportional <strong>to</strong> area, it can be<br />

appreciably higher at the input end of a brass or wind<br />

instrument than at its flared output end. The flared bore<br />

of a brass instrument or the horn on an old wind-up<br />

gramophone can therefore be considered as an acoustic<br />

transformer, which improves the match between the high<br />

impedance of the vibrating source of sound <strong>to</strong> the much<br />

lower impedance presented by air at the end of the instrument.<br />

There is clearly an optimum matching, which<br />

enhances the radialed sound without serious degredation<br />

of the excited resonant modes.<br />

Acoustic Radiation<br />

In elementary textbook treatments, the pressure at the<br />

endofanopenpipeisassumed<strong>to</strong>bezeroandtheflow<br />

rate a maximum, so that Zclosed = p/U = 0. However,<br />

in practice, the oscilla<strong>to</strong>ry motion of the air extends<br />

1<br />

0.1<br />

0.01<br />

0.001<br />

ρc0<br />

π a 2<br />

X~ω<br />

R~ω 2<br />

0.0001<br />

0.01 0.1 1<br />

10<br />

ka<br />

Fig. 15.66 Real and imaginary components of f , the<br />

impedance at the unbaffled open end of a cylindrical tube<br />

of radius a, in units of ρc0/πa 2 ,asafunctionofka (after<br />

Beranek [15.136])<br />

–10dB<br />

–20dB<br />

–30dB<br />

θ<br />

Musical <strong>Acoustics</strong> 15.3 Wind Instruments 603<br />

ka = 0.5 ka = 1.5 ka = 3.83<br />

Fig. 15.67 Polar plots of the intensity radiation from the<br />

end of a cylindrical pipe of radius a for representative ka<br />

values, calculated by Levine and Schwinger [15.137]. The<br />

radial gradations are in units of 10 dB. The intensities in the<br />

forward direction (θ = 0) relative <strong>to</strong> those of an isotropic<br />

source are 1.1, 4.8 and 11.8dB(Beranek [15.136])<br />

somewhat beyond the open end, providing a pulsating<br />

source that radiates sound, as described by Rayleigh<br />

([15.3] Vol. 1, Sect. 313). Such effects can be described<br />

by a complex terminating load impedance, ZL = R + jx.<br />

Figure 15.66 shows the real (radiation resistance) R and<br />

imaginary (inertial end-correction) x components of ZL<br />

as a function of ka, wherea is the radius of the openended<br />

pipe. The impedance is normalised <strong>to</strong> the tube<br />

impedance pc0/πa 2 .<br />

When ka ≪ 1, the reactive component is proportional<br />

<strong>to</strong> ka and corresponds <strong>to</strong> an effective increase in<br />

the tube length or end-correction of 0.61a. At low frequencies,<br />

the real part of the impedance represents the<br />

radiation resistance Rrad = ρc/4S(ka) 2 .Inthisregime,<br />

the sound will be radiated isotropically as a monopole<br />

source of strength U e iωt , illustrated in Fig. 15.67 by the<br />

polar plots of sound intensity as a function of angle and<br />

frequency.<br />

When ka is of the order of and greater than unity,<br />

the real part of the impedance approaches that of a plane<br />

wave acting across the same area as that of the tube.<br />

Almost all the energy incident on the end of the tube is<br />

then radiated and little is reflected. For ka ≫ 1, sound<br />

would be radiated from the end of the pipe as a beam<br />

of sound waves. The transition from isotropic <strong>to</strong> highly<br />

directional sound radiation is illustrated for a sequence<br />

of ka values in Fig. 15.67. The ripples in the impedance<br />

in Fig. 15.66 arise from diffraction effects, when the<br />

wavelength becomes comparable with the tube diameter.<br />

For all woodwind and brass instruments, there is<br />

therefore a crossover frequency fc ∼ c0/2πa, below<br />

which incident sound waves are reflected at the open<br />

end <strong>to</strong> form standing waves. Above fc waves generated<br />

by the reed or vibrating lips will be radiated from the<br />

ends of the instrument strongly with very little reflec-<br />

Part E 15.3

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