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Introduction to Acoustics

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Doppler-shifted frequency spectrum<br />

(measured by moving array)<br />

f = fh 0 – um<br />

2π kx 0<br />

P(kx 0 ,yh,zh)<br />

fh 0<br />

f<br />

Acoustic Holography 26.2 Acoustic Holography: Measurement, Prediction and Analysis 1087<br />

P(xh; f )<br />

Um<br />

Q ( f )<br />

De-Dopplerization<br />

Fig. 26.18 De-Dopplerization procedure for a line spectrum<br />

Stationary<br />

source Microphone array<br />

xh<br />

Reference R ( f )<br />

Wave number spectrum<br />

P(kx ,yh,zh) 0<br />

X-directional wave number spectrum of actual sound field<br />

can be regarded as sum of plane wave number spectra<br />

Radiation circle<br />

ky<br />

kx<br />

Radiation circle<br />

ky<br />

kx<br />

·<br />

Plane wave<br />

component in wave<br />

number plane<br />

p<br />

p<br />

·<br />

·<br />

y<br />

y<br />

Spatial distribution<br />

of each plane wave<br />

field<br />

x<br />

x<br />

kx 0<br />

kx 0 /2<br />

+ ···<br />

=<br />

+<br />

2πA0<br />

2πA1<br />

X-directional wave<br />

number spectra of<br />

each plane wave<br />

kx<br />

kx<br />

kx<br />

kx<br />

kx = 0 2π ( fh – f ) 0<br />

um<br />

Stationary<br />

source<br />

Frequency spectrum (measured<br />

by reference microphone)<br />

fh 0<br />

Doppler shifted spectrum<br />

of actual sound field<br />

A0<br />

fh 0<br />

fh 0 –(um/2π) kx 0 fh 0<br />

A1<br />

=<br />

+<br />

fh 0 –(um/2π)(kx 0 /2) fh 0<br />

Fig. 26.19 The continuous scanning method for a more general case (one-dimensional illustration)<br />

Moving microphone<br />

xh xm<br />

+ ···<br />

um<br />

Doppler shifted<br />

frequency spectra<br />

of each plane wave field<br />

f<br />

f<br />

f<br />

f<br />

x<br />

Part H 26.2

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