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Introduction to Acoustics

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so the time-averaged incident energy is <strong>to</strong>tally reflected.<br />

Acoustic energy is present in the second fluid, but its<br />

time average over a wave period stays constant once the<br />

steady state is reached.<br />

3.10.3 Theory of the Impedance Tube<br />

Impedance tubes are commonly used in the measurement<br />

of specific acoustic impedances; the underlying<br />

theory [3.66, 67] is based for the most part on (3.295),<br />

(3.296), and (3.297) above. The incident and the reflected<br />

waves propagate along the axis of a cylindrical<br />

tube with the sample surface at one end. A loudspeaker<br />

at the other end creates a sinusoidal pressure disturbance<br />

that propagates down the tube. Reflections from the<br />

end covered with the test material create an incomplete<br />

standing-wave pattern inside the tube.<br />

The wavelength of the sound emitted by the source<br />

can be adjusted, but it should be kept substantially<br />

larger than the pipe diameter, so that the plane wave<br />

assumption holds. With kx identified as being 0, the<br />

complex amplitude that corresponds <strong>to</strong> the sum of the<br />

incident and reflected waves has an absolute magnitude<br />

given by<br />

| ˆp|=| f ˆ||1<br />

+ Êe 2iky | , (3.309)<br />

where y is now the distance in front of the sample. The<br />

second fac<strong>to</strong>r varies with y and repeats at intervals of<br />

a half-wavelength, and varies from a minimum value of<br />

1 −|Ê| <strong>to</strong> a maximum value of 1 +|Ê|. Consequently,<br />

y<br />

y<br />

ymax, 2<br />

Incident<br />

Reflected<br />

ymin, 1<br />

Sample<br />

ymax, 1<br />

(p 2 )av<br />

(p 2 )av, max<br />

(p 2 )av, min<br />

Fig. 3.20 Incident and reflected waves inside an impedance<br />

tube. The time-averaged pressure within the tube has minimum<br />

and maximum values whose ratio depends on the<br />

impedance of the sample at the end. Another measured parameter<br />

is the distance back from the sample at which the<br />

first maximum occurs<br />

Basic Linear <strong>Acoustics</strong> 3.10 Reflection and Transmission 63<br />

the ratio of the peak acoustic pressure amplitude | ˆp|max<br />

(which occurs at one y-position) <strong>to</strong> the minimum acoustic<br />

pressure amplitude | ˆp|min (which occurs at a position<br />

a quarter-wavelength away) determines the magnitude<br />

of the reflection coefficient via the relation<br />

| ˆp|min<br />

=<br />

| ˆp|max<br />

1 −|Ê|<br />

. (3.310)<br />

1 +|Ê|<br />

The phase δ of the reflection coefficient can be<br />

determined with use of the observation that the peak<br />

amplitudes occur at y-values where δ + 2ky is an integer<br />

multiple of 2π, while the minimum amplitudes occur<br />

where it is π plus an integer multiple of 2π. Once the<br />

magnitude and phase of the reflection coefficient are determined,<br />

the specific acoustic impedance can be found<br />

from (3.296)and(3.297).<br />

3.10.4 Transmission through Walls<br />

and Slabs<br />

The analysis of transmission of sound through a wall or<br />

a partition [3.68] is often based on the idealization that<br />

the wall is of unlimited extent.<br />

If the incoming plane wave has an angle of incidence<br />

θI and if the fluid on the opposite side of the wall has the<br />

same sound speed, then the trace velocity matching principle<br />

requires that the transmitted wave be propagating<br />

in the same direction.<br />

A common assumption when the fluid is air is that<br />

the compression in the wall is negligible, so the wall is<br />

treated as a slab that has a uniform velocity vsl throughout<br />

its thickness. The slab moves under the influence<br />

of the incident, reflected, and transmitted sound fields<br />

according <strong>to</strong> the relation (corresponding <strong>to</strong> New<strong>to</strong>n’s<br />

θI<br />

nI<br />

pfront<br />

vfront<br />

vback<br />

pback<br />

Fig. 3.21 Transmission of an incident plane wave through<br />

a thin flexible slab<br />

Part A 3.10

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