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Introduction to Acoustics

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The auxiliary internal variables that enter here satisfy<br />

the supplemental relaxation equations<br />

∂pν<br />

∂t =−1 (pν − pac) . (3.219)<br />

τν<br />

Here the notation is such that the pν are given in terms<br />

of previously introduced quantities by<br />

pν = ξ ′ ν /nν . (3.220)<br />

The sound speed increments that appear in (3.218)<br />

represent the combinations<br />

(∆c)ν = 1/2aνnνc 2 . (3.221)<br />

Equations (3.218) and(3.219) are independent of<br />

the explicit physical interpretation of the relaxation processes.<br />

Insofar as acoustic propagation is concerned, any<br />

relaxation process is characterized by two parameters,<br />

the relaxation time τν and the sound speed increment<br />

(∆c)ν. The various parameters that enter in<strong>to</strong> the irreversible<br />

thermodynamics formulation of (3.214) through<br />

(3.216) affect the propagation of sound only as they enter<br />

in<strong>to</strong> the values of the relaxation times and of the sound<br />

speed increments. The replacement of internal variables<br />

by quantities pν with the units of pressure implies no<br />

assumption as <strong>to</strong> the precise nature of the relaxation<br />

process. [An alternate formulation for a parallel class<br />

of relaxation processes concerns structural relaxation<br />

[3.55]. The substance can locally have more than one<br />

state, each of which has a different compressibility. The<br />

internal variables are associated with the deviations of<br />

the probabilities of the system being in each of the states<br />

from the probabilities that would exist were the system<br />

in quasistatic equilibrium. The equations that result are<br />

mathematically the same as (3.218)and(3.219).]<br />

The attenuation of plane waves governed by (3.218)<br />

and (3.219) is determined when one inserts substitutions<br />

of the form of (3.200)forpac and the pν. The relaxation<br />

equations yield the relations<br />

1<br />

ˆpν = ˆpac . (3.222)<br />

1 − iωτν<br />

These, when inserted in<strong>to</strong> the complex amplitude<br />

version of (3.218), yield the dispersion relation<br />

k 2 = ω2<br />

c2 �<br />

1 + i 2ωδcl �<br />

�<br />

2(∆c)ν iωτν<br />

+ .<br />

c2 c 1 − iωτν<br />

ν<br />

(3.223)<br />

To first order in the small parameters, δcl and (∆c)ν,this<br />

yields the complex wavenumber<br />

k = ω<br />

�<br />

1 + i<br />

c<br />

ωδcl �<br />

�<br />

(∆c)ν iωτν<br />

+ , (3.224)<br />

c2 c 1 − iωτν<br />

ν<br />

1<br />

0.8<br />

0.6<br />

0.4<br />

0.2<br />

(αv λ)/(αv λ)m<br />

Basic Linear <strong>Acoustics</strong> 3.7 Attenuation of Sound 51<br />

0<br />

0.06 0.1 0.2 0.4 0.6 1 2 4 6 10 20 40<br />

f/fv<br />

Fig. 3.11 Attenuation per wavelength (in terms of characteristic<br />

parameters) for propagation in a medium with a single<br />

relaxation process. Here the wavelength λ is 2πc/ω, and<br />

the ratio f/ fν of frequency <strong>to</strong> relaxation frequency is ωτν.<br />

The curve as constructed is independent of c and (∆c)ν<br />

which corresponds <strong>to</strong> waves propagating in the +xdirection.<br />

The attenuation coefficient, determined by the<br />

imaginary part of (3.224), can be written<br />

α = αcl + �<br />

αν . (3.225)<br />

ν<br />

The first term is the classical attenuation determined by<br />

(3.203). The remaining terms correspond <strong>to</strong> the incremental<br />

attenuations produced by the separate relaxation<br />

processes, these being<br />

αν = (∆c)ν<br />

c 2<br />

ω2τν . (3.226)<br />

1 + (ωτν) 2<br />

Any such term increases quadratically with frequency<br />

at low frequencies, as would be the case for classical<br />

absorption (with an increased bulk viscosity), but<br />

it approaches a constant value at high frequencies.<br />

The labeling of the quantities (∆c)ν as sound speed<br />

increments follows from an examination of the real part<br />

of the complex wavenumber, given by<br />

kR = ω<br />

c<br />

�<br />

1 − �<br />

ν<br />

(∆c)ν<br />

c<br />

(ωτν) 2<br />

1 + (ωτν) 2<br />

�<br />

. (3.227)<br />

The ratio, of ω <strong>to</strong> kR, is identified as the phase velocity<br />

vph of the wave. In the limit of low frequencies, the phase<br />

velocity predicted by (3.227) is the quantity c, whichis<br />

the sound speed for a quasi-equilibrium process. In the<br />

limit of high frequencies, however, <strong>to</strong> first order in the<br />

(∆c)ν, the phase velocity approaches the limit<br />

vph → c + �<br />

(∆c)ν . (3.228)<br />

ν<br />

Consequently, each (∆c)ν corresponds <strong>to</strong> the net increase<br />

in phase velocity of the sound wave that occurs<br />

Part A 3.7

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