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

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CHAPTER 4. FINGER HOLE IMPEDANCE SPECTRA AND LENGTH CORRECTIONS 55<br />

4.2.3 Calibration<br />

4.2.3.1 Calibration <strong>of</strong> impedance heads<br />

Each impedance head is calibrated separately against known impedance loads, using the<br />

methods described in §3.4.2 with some modifications. Most importantly, since the reference<br />

plane for each head is 50 mm further from the microphones than the coupling point, the ‘infinite<br />

impedance’ <strong>and</strong> the ‘infinite flange’ calibration loads are in reality pipes <strong>of</strong> length 50 mm<br />

with the appropriate termination. Further, in §3.4.2, we were only interested in measuring the<br />

input impedance rather than pressure <strong>and</strong> flow. Consequently, only three calibration loads<br />

were required <strong>and</strong> one element (A 11 ) in the matrix A was left undetermined, with no effect on<br />

impedance <strong>measurement</strong>s. In determining the equivalent circuit for a finger hole, pressure<br />

<strong>and</strong> flow differences enter into the equations, so the impedance heads should be calibrated<br />

absolutely for pressure <strong>and</strong> flow.<br />

This can be achieved by flush-mounting a reference microphone in the infinite impedance<br />

calibration load. Assuming that the microphone has negligible compliance, the elements A j 1<br />

are derived from the pressure p measured at the face <strong>of</strong> this impedance load as<br />

A j 1 = b j /p (4.3)<br />

where, as in (3.7), b j is the signal from microphone j (j = 1,2,...,n where n is the number <strong>of</strong><br />

microphones). The remaining elements in A are determined using the methods <strong>of</strong> §3.4.2 from<br />

<strong>measurement</strong>s <strong>of</strong> the semi-infinite pipe <strong>and</strong> the infinite flange calibration loads.<br />

4.2.3.2 Calibration <strong>of</strong> entire system<br />

The two heads are attached to either end <strong>of</strong> a 100 mm tube with no finger hole (thereby<br />

sharing the same reference plane). For this configuration, p 1 = p 2 <strong>and</strong> U 1 = −U 2 (the sign difference<br />

is a consequence <strong>of</strong> the definition <strong>of</strong> positive flow being into the <strong>measurement</strong> load).<br />

However, allowing for small differences in the microphones comprising each array, the measured<br />

pressures <strong>and</strong> flows may be somewhat different. This is accounted for by making small<br />

changes to the matrix A for each head.<br />

A <strong>measurement</strong> <strong>of</strong> each <strong>of</strong> Z s <strong>and</strong> Z a is performed on the ‘no-hole’ system. In each case, the<br />

pressure at the reference plane p is taken as the mean <strong>of</strong> the pressure seen by each <strong>measurement</strong><br />

head at the reference plane. Likewise the flow U is taken as the mean <strong>of</strong> the flows (with a<br />

sign change due to the way flow is defined). Then for each head we have the following matrix<br />

equation:<br />

A<br />

[ ]<br />

ps p [<br />

a<br />

=<br />

Z 0 U s Z 0 U a<br />

c s c a<br />

], (4.4)<br />

where c s <strong>and</strong> c a are the vectors <strong>of</strong> microphone signals obtained during the <strong>measurement</strong> <strong>of</strong> Z s<br />

<strong>and</strong> Z a respectively. This equation may be solved for the matrices A for each head.<br />

The splitting ratio r may also be improved by calibration. As mentioned above, the voltage<br />

signal applied to each loudspeaker is V r or V r<br />

. The pressure <strong>and</strong> flow at the reference plane, p

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