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Introduction to Acoustics

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y bowed, plucked and struck stringed instruments and<br />

all percussion instruments.<br />

Time-Domain Measurements<br />

The vibrational characteristics of an instrument can also<br />

be investigated in the time domain. For example, by<br />

striking a stringed instrument with a light hammer or<br />

exciting the vibrational modes of a woodwind or brass<br />

instrument with a short puff of air, the frequencies of<br />

free vibration of the vibrational modes and their damping<br />

can be determined from their time-dependent decay.<br />

Provided the damping is not <strong>to</strong>o strong (Q ≫1), the<br />

modes will decay with time as<br />

ξn(t) = ξ0 e −t/τn e iωnt , (15.5)<br />

where τn = 2Qn/ωn = Qn/π fn. The frequency fn of<br />

a given mode can be determined from its inverse period<br />

and Qn from π× the number of periods for the amplitude<br />

<strong>to</strong> fall by the fac<strong>to</strong>r exponential e. The Q-value<br />

of strongly excited modes of a musical instrument can<br />

be estimated from τ60dB = 13.6τ, the Sabine decay time<br />

(Chap. 10 Concert Hall <strong>Acoustics</strong>). This is the perceptually<br />

significant time taken for the sound pressure <strong>to</strong> fall<br />

by a fac<strong>to</strong>r of 10 3 – from a very loud level <strong>to</strong> just being<br />

detectable. Hence, Qn = π fnτ60/13.6 ∼ 0.23 fnτ60.<br />

For example, the sound of a strongly plucked cello<br />

open A-string (220 Hz) can be heard for at least ∼ 2s,<br />

corresponding <strong>to</strong> a Q-value of ≈ 100 or more.<br />

Damping results in a loss of s<strong>to</strong>red energy given by<br />

dEn<br />

dt =−ωn En =−2<br />

Qn<br />

En<br />

. (15.6)<br />

τn<br />

Hence, the power P required <strong>to</strong> maintain a constant<br />

amplitude at resonance is ωn<br />

Qn En, whereEnis the energy<br />

s<strong>to</strong>red. This tends <strong>to</strong> be the way that Q is defined<br />

and measured by physicists, whereas in acoustic spectroscopy<br />

it is more usual <strong>to</strong> define and measure Q-values<br />

from either the width of resonances in spectroscopic<br />

measurements or from decay times after transient excitation.<br />

As illustrated above, all such definitions are<br />

equivalent.<br />

15.1.2 Radiation from Instruments<br />

Although a large number of vibrational modes of a musical<br />

instrument may be excited simultaneously, they will<br />

not be equally important in radiating sound, which has<br />

important consequences for the quality of the sound.<br />

This section therefore provides a brief introduction <strong>to</strong><br />

the radiation of sound from the vibrational modes of<br />

musical instruments.<br />

Musical <strong>Acoustics</strong> 15.1 Vibrational Modes of Instruments 537<br />

Sound Waves in Air<br />

In free space, the longitudinal displacement ξ(x, t) =<br />

ξ0 e i(ωt−kx) of plane sound waves satisfies the wave<br />

equation<br />

∂2ξ 1<br />

=<br />

∂x2 c2 ∂<br />

0<br />

2ξ . (15.7)<br />

∂t2 The dispersionless (independent of frequency) velocity<br />

of sound c0 = √ γ P0/ρ, whereγ (≈ 1.4) is the ratio<br />

of specific heats at constant pressure and volume, P0<br />

(≈ 10 5 Pa or N/m 2 ) is the ambient pressure and ρ<br />

(≈ 1kg/m 3 ) is the density (the brackets give the values<br />

for air at ambient pressure and temperature). The ratio<br />

of acoustic pressure p =−γ P0∂ξ/∂x <strong>to</strong> the particle velocity<br />

v = ∂ξ/∂t is referred <strong>to</strong> as the specific impedance,<br />

z0 = p/v = ρc0.<br />

The appearance of γ in the expression for the velocity<br />

of sound reflects the adiabatic nature of acoustic<br />

waves. This arises because acoustic wavelengths are<br />

far <strong>to</strong>o long <strong>to</strong> allow any significant equalisation of<br />

the longitudinal temperature fluctuations arising from<br />

the compressions and rarefactions of a sound wave. In<br />

free space longitudinal heat flow between the fluctuating<br />

regions is only important at very high ultrasonic frequencies<br />

(MHz), where it leads <strong>to</strong> significant attenuation. The<br />

major source of attenuation of freely propagating acoustic<br />

sound waves arises from the water vapour present.<br />

However, both viscous and transverse thermal losses <strong>to</strong><br />

the side walls of woodwind and brass instruments can<br />

result in significant attenuation, as described later.<br />

The above expressions neglect first-order, nonlinear,<br />

corrections <strong>to</strong> the compressibility, proportional <strong>to</strong><br />

∂ξ/∂x, and other inertial correction terms in the nonlinear<br />

Navier–S<strong>to</strong>kes equation. This approximation breaks<br />

down at the very high intensities in the bores of the<br />

trumpet and trombone when played very loudly [15.9],<br />

which results in shockwave propagation, with a transition<br />

from a relatively smooth <strong>to</strong> a very brassy sound (son<br />

cuivré in French). For the present, such corrections will<br />

be neglected.<br />

The speed of sound in air depends on the temperature<br />

θ (degrees centigrade) and, <strong>to</strong> a lesser extent, on the<br />

humidity. For 50% humidity,<br />

c0(θ) = 332 (1 + θ/273) 1/2 ≈ 332(1 + 1.710 −3 θ) ,<br />

(15.8)<br />

giving a value of 343 m/s at20 ◦ C. Note that the air<br />

inside a woodwind or brass instrument, once the instrument<br />

is warmed up, will always be warm and humid,<br />

which will affect the playing pitch.<br />

Part E 15.1

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