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Introduction to Acoustics

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ubble natural acoustic resonance ω2 0 , and the expression<br />

for the scattered field from an acoustic bubble under an<br />

incident pressure field at frequency ω.<br />

The acoustic resonance in the linear regime of a sin-<br />

gle bubble of radius a is:<br />

ω 2 0 =<br />

�<br />

3γ p0<br />

2T<br />

+ (3γ − 1)<br />

ρwa2 ρwa3 �<br />

, (5.14)<br />

where p0 is the ambient pressure outside the bubble,<br />

T is surface tension (tensile force/length in units<br />

N/m), ρw is the density of water and γ is the ratio<br />

of specific heats. Neglecting surface tension in (5.14)<br />

for bubble sizes larger than 1 µm and considering the<br />

acoustic expansion/compression process <strong>to</strong> be adiabatic<br />

(c 2 air = γ p0/ρair), we obtain the approximate expression<br />

ω0 = 1<br />

a<br />

�<br />

3c 2 air ρair<br />

ρw<br />

, (5.15)<br />

and for cair � 340 m/s, we get f0 � 3 a with a in m and<br />

f0 in Hz.<br />

We now consider an incident plane wave at frequency<br />

ω in the regime ka = ωa/c = 2πa/λ ≪ 1. The<br />

far-field expression for the spatial part of the radiated<br />

acoustic field pr is<br />

pr(r) =− a<br />

r pi<br />

�<br />

exp − iω<br />

�<br />

(r − a)<br />

c<br />

�<br />

× 1 − ω2 0<br />

ω2 �<br />

1 − iωa<br />

�<br />

c<br />

�−1 . (5.16)<br />

First, we note that in the high-frequency limit, we recover<br />

pr(r, t) =− a r pi<br />

� � r−a<br />

t − c that was given by the<br />

boundary conditions at the bubble surface.<br />

To understand the effect of the resonance frequency,<br />

consider two cases. The first case is ω ≫ ω0 for which<br />

we obtain:<br />

pr(r) =− a<br />

r pi e − iω c (r−a) , (5.17)<br />

whereas for the case ω = ω0 we get:<br />

pr(r) =− ic<br />

ωr pi e − iω c (r−a) =− iλ<br />

2πr pi e − iω c (r−a) .<br />

(5.18)<br />

Comparing the two equations, (5.18) appears <strong>to</strong> be the<br />

field radiating from a sphere of radius λ/2π which is<br />

much larger than a. For example, neglecting surface<br />

tension, at 1 atm, ω0a ≈ 20 so that λ ≈ 500a. This resonance<br />

effect is also quite apparent when considering the<br />

scattering cross section of the bubble.<br />

a)<br />

0<br />

1<br />

2<br />

3<br />

4<br />

5<br />

6<br />

1480<br />

Depth (km)<br />

c)<br />

80<br />

70<br />

Underwater <strong>Acoustics</strong> 5.2 Physical Mechanisms 163<br />

Critical depth<br />

= 4420m<br />

Bot<strong>to</strong>m = 5322m<br />

b)<br />

250Hz<br />

500Hz 150Hz 100Hz<br />

50Hz<br />

25Hz<br />

18Hz<br />

100Hz<br />

1500 1520 1540 50 60 70 80 90<br />

Sound velocity (m/s) Spectrum level (dB re 1Pa)<br />

Spectrum level (dB/Pa/sterad)<br />

3781m<br />

713m<br />

–20 –10 0 10 20<br />

Down Up<br />

Elevation angle (deg)<br />

Fig. 5.16a–c Noise in the deep ocean. (a) Sound-speed profile and<br />

(b) noise level as a function of depth in the Pacific (after [5.30]).<br />

(c) The vertical directionality of noise at the axis of the deep sound<br />

channel and at the critical depth in the Pacific (after [5.31])<br />

The scattering cross section σs is the ratio of the <strong>to</strong>tal<br />

scattered power (intensity × area = pressure × velocity<br />

× enclosing area) <strong>to</strong> the incident plane-wave intensity<br />

(given by p 2 i /2ρwc, with the fac<strong>to</strong>r of 1/2 coming from<br />

averaging over a cycle) and therefore has the units of<br />

area. We perform this calculation in the far field using<br />

(5.16) <strong>to</strong> obtain<br />

σs =<br />

�<br />

1 − ω2 0<br />

ω 2<br />

4πa 2<br />

� � iωa<br />

1 − c<br />

�2 ω=ω0<br />

−→ λ2<br />

, (5.19)<br />

π<br />

which is consistent with a surface area associated with<br />

the discussion below (5.18). The resonance makes the<br />

bubble appear larger in surface area than its dimension.<br />

On the other hand, for the case ω ≪ ω0,wehave<br />

σs = 4πa 2<br />

� �4 ω<br />

, (5.20)<br />

ω0<br />

Part A 5.2

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