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Introduction to Acoustics

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ω ′ = 0, and this is consistent with kR being odd in ω and<br />

representable locally as a power series. Validity also requires<br />

that kI/ω2 be finite at ω = 0, which is consistent<br />

with the relaxation models mentioned in the section below.<br />

The existence of the integral also places a restriction<br />

on the asymp<strong>to</strong>tic dependence of kR as ω →∞.<br />

A possible consequence of the last relation is that<br />

�<br />

kI(ω)<br />

lim<br />

ω→∞ ω2 �<br />

� �<br />

kI(ω)<br />

=<br />

+ 2<br />

π<br />

ω 2<br />

�<br />

0<br />

∞<br />

0<br />

[kR(ω ′ )/ω ′ ]−[kR(ω ′ )/ω ′ ]0<br />

ω ′2<br />

dω ′ . (3.253)<br />

The validity of this requires that the integral exists, which<br />

is so if the phase velocity approaches a constant at high<br />

frequency. An implication is that the attenuation must<br />

approach a constant multiplied by ω 2 at high frequency,<br />

where the constant is smaller than that at low frequency<br />

if the phase velocity at high frequency is higher than that<br />

at low frequency.<br />

Imaginary Part Within the Integrand<br />

Analogous results, only with the integration over the<br />

imaginary part of k, result when k/ω is replaced by k in<br />

(3.247). Doing so yields<br />

�∞<br />

kI(ω)<br />

2Pr � �� � dω<br />

ω2 − ω2 1 ω2 − ω2 2<br />

0<br />

π<br />

=<br />

ω2 1 − ω2 �<br />

kR(ω1)<br />

−<br />

ω1 2<br />

kR(ω2)<br />

�<br />

, (3.254)<br />

ω2<br />

which in turn yields<br />

kR(ω)<br />

ω<br />

= kR(ω1)<br />

−<br />

ω1<br />

2(ω2 1 − ω2 )<br />

π<br />

�∞<br />

kI(ω<br />

×Pr<br />

′ )<br />

(ω ′2 − ω2 1 )(ω′2 − ω2 ) dω′ . (3.255)<br />

0<br />

Then, taking of the limit ω1 → 0, one obtains<br />

kR(ω)<br />

ω<br />

� �<br />

kR(ω)<br />

=<br />

ω<br />

0<br />

+ 2ω2<br />

π Pr<br />

�∞<br />

0<br />

kI(ω ′ )<br />

ω ′2 (ω ′2 − ω 2 ) dω′ .<br />

(3.256)<br />

Basic Linear <strong>Acoustics</strong> 3.7 Attenuation of Sound 55<br />

This latter expression requires that kI/ω 2 be integrable<br />

near ω = 0.<br />

Attenuation Proportional <strong>to</strong> Frequency<br />

Some experimental data for various materials suggest<br />

that, for those materials, kI is directly proportional <strong>to</strong> ω<br />

over a wide range of frequencies. The relation (3.256)is<br />

inapplicable if one seeks the corresponding expression<br />

for phase velocity. Instead, one uses (3.255), treating ω1<br />

as a parameter. If one inserts<br />

kI(ω) = Kω (3.257)<br />

in<strong>to</strong> (3.255), the resulting integral can be performed<br />

analytically, with the result<br />

kR(ω) kR(ω1)<br />

= −<br />

ω ω1<br />

2<br />

� �<br />

ω<br />

K ln . (3.258)<br />

π ω1<br />

(The simplest procedure for deriving this is <strong>to</strong> replace<br />

the infinite upper limit by a large finite number and<br />

then separate the integrand using the method of partial<br />

fractions. After evaluation of the individual terms, one<br />

takes the limit as the upper limit goes <strong>to</strong> infinity, and<br />

discovers appropriate cancelations.) The properties of<br />

the logarithm are such that the above indicates that the<br />

quantity<br />

kR(ω) 2<br />

+ K ln(ω) = constant (3.259)<br />

ω π<br />

is independent of ω. This deduction is independent of<br />

the choice of ω1, but the analysis does not tell one what<br />

the constant should be. A concise restating of the result<br />

is that there is some positive number ω0, such that<br />

kR(ω) 2<br />

� �<br />

ω0<br />

= K ln . (3.260)<br />

ω π ω<br />

The result is presumably valid at best only over the range<br />

of frequencies for which (3.257) is valid. Since negative<br />

phase velocities are unlikely, it must also be such that<br />

the parameter ω0 is above this range. This approximate<br />

result also predicts a zero phase velocity in the limit of<br />

zero frequency, and this is also likely <strong>to</strong> be unrealistic.<br />

But there may nevertheless be some range of frequencies<br />

for which both (3.257) and(3.260) would give a good<br />

fit <strong>to</strong> experimental data.<br />

3.7.5 Attenuation of Sound in Air<br />

In air, the relaxation processes that affect sound attenuation<br />

are those associated with the (quantized) internal<br />

vibrations of the dia<strong>to</strong>mic molecules O2 and N2. The<br />

ratio of the numbers of molecules in the ground and<br />

Part A 3.7

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