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Introduction to Acoustics

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propagating from a central point. Such waves satisfy<br />

the wave equation, which may be written in spherical<br />

coordinates as<br />

∇ 2 (rp) = 1<br />

c2 ∂<br />

0<br />

2 (rp)<br />

∂t2 . (15.101)<br />

We therefore have standing-wave solutions for rp that<br />

are very similar <strong>to</strong> those of a cylindrical tube, with<br />

sin kr<br />

p = C e<br />

r<br />

iωt . (15.102)<br />

Note that the pressure remains finite at the apex of the<br />

cone, r = 0, where sin(kr)/r → k. For a conical tube<br />

with a pressure node p = 0 at the open end, we therefore<br />

have standing wave modes with kn L = nπ and<br />

fn = nc0/2L,wherenis any integer. The frequencies of<br />

the excited modes are therefore identical <strong>to</strong> the modes<br />

of a cylindrical tube of the same length that is open at<br />

both ends. The lowest note at f1 = c0/2L for a conical<br />

tube instrument with a reed at one end (e.g. the oboe and<br />

saxophone) is therefore an octave above a reed instrument<br />

of the same length with a cylindrical bore (e.g. the<br />

clarinet) with a fundamental frequency of c0/4L.<br />

The flow velocity U is determined by the acceleration<br />

of the air resulting from the spatial variation of the<br />

pressure, so that<br />

ρ ∂U<br />

∂t = ∂(r2 p)<br />

∂r = C (sin kr + kr cos kr) eiωt .<br />

(15.103)<br />

Figure 15.71 illustrates the pressure and flow velocity<br />

for the n = 5 mode of a conical tube. Unlike the modes<br />

of cylindrical tube, the nodes of U no longer coincide<br />

with the peaks in p, which is especially apparent for<br />

the first few cycles along the tube. Furthermore, the<br />

amplitude fluctuations increase with distance r from the<br />

apex (∼ r), whilst the fluctuations in pressure decrease<br />

≈ 1/r. A conical section therefore acts as an acoustic<br />

transformer helping <strong>to</strong> match the high impedance at the<br />

input mouthpiece end <strong>to</strong> the low impedance at the output<br />

radiating end.<br />

Attaching a mouthpiece or reed <strong>to</strong> the end of a conical<br />

tube requires truncation of the cone, which will<br />

clearly perturb the frequencies of the harmonic modes.<br />

However, using a mouthpiece or reed unit having the<br />

same internal volume as the volume of the truncated<br />

section removed will leave the frequencies of the lowest<br />

modes unchanged. Only when the acoustic wavelength<br />

becomes comparable with the length of truncated section<br />

will the perturbation be large.<br />

20<br />

15<br />

10<br />

5<br />

0<br />

–5<br />

–10<br />

–15<br />

Pressure p<br />

Musical <strong>Acoustics</strong> 15.3 Wind Instruments 607<br />

Flow U<br />

–20<br />

0 0.2 0.4 0.6 0.8 1<br />

r/L<br />

Fig. 15.71 Pressure and flow velocity of the n = 5 mode<br />

along the length of a conical tube<br />

Fletcher and Rossing ([15.5], Sect. 8.7) consider the<br />

physics of the truncated conical tube and give the input<br />

impedance derived by Olson [15.139]<br />

� �<br />

Zin = ρc0<br />

S1<br />

� �<br />

sin(kL−θ2) ρc0<br />

iZL sin + sin kL<br />

θ2 S2<br />

ZL sin(kL+θ1−θ2)<br />

� � ,<br />

ρc0 sin(kl+θ1)<br />

sin θ1 sin + j θ2 S2 sin θ1<br />

(15.104)<br />

where x1 and x2 are the distances of the two ends from<br />

the apex of the truncated conical section. The length L =<br />

x2 − x1, the end areas are S1 and S2, with θ1 = tan −1 kx1<br />

and θ2 = tan −1 kx2.<br />

a) b)<br />

Resonant frequencies<br />

4<br />

3<br />

2<br />

1<br />

0.01 0.1 1.0<br />

Input/output diameters<br />

0.01 0.1 1.0<br />

Input/output diameters<br />

Fig. 15.72a,b The first four resonant frequencies of truncated<br />

cones with (a) both ends open, and (b) the input end<br />

closed, as a function of the ratio of their input <strong>to</strong> output<br />

diameters (after Ayers et al. [15.138])<br />

Part E 15.3

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