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Flute acoustics: measurement, modelling and design - School of ...

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42 CHAPTER 3. MEASURING ACOUSTIC IMPEDANCE<br />

angular frequency <strong>and</strong> the air density. This treatment assumes that all higher modes excited at<br />

the reference plane are evanescent <strong>and</strong> do not couple to any higher modes in other parts <strong>of</strong> the<br />

object.<br />

Incidentally, we may rewrite (3.11) in terms <strong>of</strong> the pressure <strong>and</strong> flow. The plane-wave flow<br />

is continuous at a duct discontinuity (U true = U meas = U) <strong>and</strong> so the true plane wave pressure is<br />

given by<br />

N∑<br />

p true ≈ p meas −U (F 0,n ) 2 Z n,n (c) . (3.13)<br />

For the case <strong>of</strong> an axially symmetric impedance head comprised <strong>of</strong> an acoustic resistance<br />

<strong>of</strong> annular cross section <strong>and</strong> a microphone, both located at the reference plane, Fletcher et al.<br />

(2005) provide an equation similar to (3.11):<br />

Z true ≈ Z meas −<br />

n=1<br />

n=1<br />

N∑ ωρ<br />

J 0 ( α na<br />

), (3.14)<br />

2πk n M n R<br />

where a <strong>and</strong> R are, respectively, the radius <strong>of</strong> the annulus <strong>and</strong> the entry radius <strong>of</strong> the object<br />

under study, <strong>and</strong> α n is the nth zero <strong>of</strong> the first-order Bessel function <strong>of</strong> the first kind. The factor<br />

M n is given by<br />

M n = R2<br />

2 J 0 2 (α n). (3.15)<br />

In both <strong>of</strong> these cases, the number <strong>of</strong> higher modes included in the sum, N, should be<br />

chosen so that the sum converges. Van Walstijn et al. used 40 <strong>and</strong> Fletcher et al. 100 higher<br />

modes to be certain <strong>of</strong> achieving a good approximation, although this will <strong>of</strong> course depend on<br />

the size <strong>of</strong> the diameter mismatch.<br />

Brass & Locke (1997) discuss the effect <strong>of</strong> the evanescent wave on impedance <strong>measurement</strong>s<br />

<strong>of</strong> the ear canal with a loudspeaker <strong>and</strong> microphone in close proximity.<br />

An impedance determined by applying the above-mentioned corrections will usually be<br />

less accurate than one measured with a matching impedance head, as turbulent losses are not<br />

taken into account in the multi-modal model.<br />

3.5.4 R<strong>and</strong>om noise (acoustical or electrical)<br />

Each transducer signal is contaminated by r<strong>and</strong>om noise. Whether this is <strong>of</strong> acoustical or electrical<br />

origin is usually unimportant. This noise <strong>of</strong>ten has an overall 1/f n -dependance, where<br />

0 < n < 1 <strong>and</strong> the quality <strong>of</strong> <strong>measurement</strong>s may be improved by increasing the power in the<br />

lower frequencies.<br />

3.5.5 The ‘singularity factor’<br />

The sensitivity <strong>of</strong> any impedance head to errors in the input quantities varies over frequency.<br />

In the two-microphone method, for example, the head becomes ‘singular’ when the microphone<br />

spacing is an integral multiple <strong>of</strong> λ/2 <strong>and</strong> in this vicinity large errors in impedance result<br />

from small <strong>measurement</strong> errors. Conversely, for a microphone spacing <strong>of</strong> λ/4, the head is<br />

least sensitive to errors in the measured quantities. This effect is conveniently represented by<br />

the function SF (for ‘singularity factor’), defined by Jang & Ih (1998, their equation (16)), <strong>and</strong>

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