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Introduction to Acoustics

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eB<br />

e1<br />

Reference<br />

signal<br />

(2)<br />

(1)<br />

SW<br />

Attenua<strong>to</strong>rs<br />

α ß<br />

B A<br />

(A–B)<br />

Inphase quadrature<br />

e2<br />

eA<br />

AC null detec<strong>to</strong>r<br />

(lock-in amplifier)<br />

Fig. 24.8 Interchange reference method (after Wong [24.29],<br />

Chap. 4)<br />

we have<br />

e2β1 cos θ − e1α1 = 0 . (24.25)<br />

Similarly, when e2 is selected as the reference by the<br />

switch at position 2, the null condition with attenua<strong>to</strong>r<br />

readings β2 and α2 provides the following:<br />

e1β2 cos θ − e2α2 = 0 . (24.26)<br />

From (24.5)and(24.6), the general equations for the<br />

amplitude ratio R = e2/e1 and cos θ are found<br />

R =[(α1/α2)(β2/β1)] 1/2 , (24.27)<br />

cos θ =[(α1α2)/(β1β2)] 1/2 . (24.28)<br />

Although for symmetry, Fig. 24.8 shows two attenua<strong>to</strong>rs,<br />

in practice only one attenua<strong>to</strong>r is required. For<br />

the condition in Fig. 24.9, wheree2 > e1, α1 = β2 = 1.<br />

24.4 Corrections<br />

24.4.1 Heat Conduction Correction<br />

The alternating sound pressure induces compression and<br />

expansion in the gas medium inside the closed cavity.<br />

At sufficiently low frequencies, the induced temperature<br />

changes occur isothermally, and the heat exchange<br />

at the walls of the cavity has <strong>to</strong> be included when computing<br />

the acoustic impedance of the cavity. As the<br />

frequency increases, heat conduction between the gas<br />

e1<br />

Microphones and Their Calibration 24.4 Corrections 1029<br />

a) With e1 as the reference b) With e2 as the reference<br />

+j<br />

+j<br />

Quadrature<br />

component<br />

(eA– eB)<br />

e1α1<br />

–j<br />

Θ<br />

e2 ß1<br />

e1<br />

e2<br />

e2<br />

Quadrature<br />

component<br />

(eA– eB)<br />

e2 α2<br />

–j<br />

Θ<br />

e1 ß2<br />

Fig. 24.9 Vec<strong>to</strong>r diagram for the in-phase null condition<br />

(after Wong [24.29], Chap. 4)<br />

The uncertainty of the attenua<strong>to</strong>r that can be a sevendecade<br />

ratio transformer (inductive voltage dividers) is<br />

of the order of 0.1 ppm. The uncertainty of the measured<br />

amplitude ratio is of the order of 1 ppm. Other circuits<br />

employing inductive voltage dividers for voltage ratio<br />

measurements are given in [24.17, 23].<br />

Reference Impedance Selection<br />

The reference impedance Zx showninFig.24.6 needs<br />

<strong>to</strong> be carefully selected. The nature of the impedance,<br />

either purely resistive or purely capacitive, or a combination<br />

of electrical impedances, dictates the mode of<br />

evaluation of the fac<strong>to</strong>r k, which is required for the computation<br />

of microphone sensitivity in (24.24). If Zx is<br />

a resistance, the angular frequency ω,shownin(24.19),<br />

has <strong>to</strong> be measured. When the impedance is a capacitance<br />

Cr the term Zx = 1/(iωCr), and the frequency<br />

terms are canceled. The numerical value of Zx is chosen<br />

such that the magnitudes of e1 and e2 are nearly equal in<br />

order <strong>to</strong> enhance the measurement of voltage ratios using<br />

null measurement techniques. For precise measurement<br />

of Zx, the capacitance of the connecting cables <strong>to</strong> the<br />

impedance should be taken in<strong>to</strong> consideration.<br />

and the walls decreases. Gradually, isothermal conditions<br />

change <strong>to</strong> adiabatic conditions, at which virtually<br />

no heat is exchanged with the walls.<br />

Classical analytical approaches <strong>to</strong> calculate heat<br />

conduction in cavities are given by Ballantine [24.2]and<br />

Daniels [24.33]. Correction fac<strong>to</strong>rs for heat conduction<br />

were obtained by Biagi and Cook [24.34]. Theoretical<br />

and experimental data, based on thermal diffusion, on<br />

the acoustic impedance of the cavity, are given by Ger-<br />

e1<br />

e2<br />

Part H 24.4

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