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Publisher’s version / Version de l'éditeur:

Journal of the Acoustical Society of America, 51, 5(pt. 2), pp. 1764-1765,

1972-01-01

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Correlation of reverberant sound fields using a k- transform technique

Donato, R. J.

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Ser

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LA CORRELATION DES CHAMPS SONORES

REVERBERANT$ BAR UNE METHODE

DE "K9' TRANSFORMES

L'auteur dCcrit une mCt11ode de transformes servant

B

calculer la correlation spatiale de divers genres de champs acoustiques. On insiste sur le fait que l'emploi d'une mCthode d e

"k"

nombres pour dCterminer un champ sonore Cquivaut

B

la synth&se d'un champ sonore en t a n t que sommation d'une sCrie d'ondes planes.

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7 -

.

, v

-J$i

r,-y--yT%:3

Rrpriiztrd frofit: The Journal of the Acoustical Society of America

11.2, 11.7; 2.7; 13.6 Received 27 September 1971

Correlation of Reverberant Sound Fields

Using a k-Transf orm Technique

Building Physics Section, Division of Bzdilding Research, National Research Council of Canada, Ottawa, Canada

A transform method is described for calculating the spatial correlation for various kinds of acoustic fields. The method emphasizes the equivalence between using a k-number approach for specifying a sound field and the synthesis of a sound field as a summation of a series of plane waves.

The usual way of determining the spatial correlation metric system, we may write the distribution as pe(B) of a three- or two-dimensional reverberant sound field where, of course,

is to decompose the original field into a system of plane

waves, calculate the effect for a small bundle of such p~(Q)dQ=pe(e)de.

waves, and then integrate for the whole set.' If we consider a three-dimensional reverberant space, Specifically, in the three-dimensional case, the corre- then

lation function p ( d , ~ ) for spatial separation d and time

pe(e) = (47r)-l27r sine

=a

sine.

difference T is given by (4)

For such an axially symmetric system we may write d C O S ~

p ( d , ~ ) = ( 4 ~ ) - ~ l '

/ox

P(T+_) s i n e d e d ~ (1) k fk(k)dk=2($ sinedo), (5) where we have now expressed the distribution in terms where c is the propagation velocity, and 8, (p are the

polar and azimuth angles in spherical coordinates; the of fk(k). Equation 5 equates the energy for a band dk factor 47r ensures normalization. When we are consider- in the k plane to that in band dB in the 8 plane.

Writing k =k, sine, where k, is the wave propagation ing sine waves we may write

number, then

and we may write Eq. 1 for T = O as Equation 6 is a measure of the power k spectrum of the sin(wd cose/c) O reverberant sound field. By taking the inverse trans-

P(~,O) = ( W 1 I

1

:7r

form-in this case Hankel transform as we have as- sumed axial symmetry-and using the Wiener-

sin(wd/c) Khintchine theorem, we may derive the correlation

-

- (3) function between two points separated in space. Thus

wd/c we may write for the spatial correlation coefficient

I. TRANSFORM METHOD

Sometimes when dealing with sound transmission problems it is more convenient to deal with the wave- number parameter k than the angle of incidence 8. The following examples emphasize the equivalence of the two approaches. The first example evaluates the three- dimensional reverberant field case given above.

A. Three-Dimensional Reverberant Field Let pn(Q) .dQ represent the distribution of energy within solid angles Q and Q+dQ. For an azimuthly sym-

1764 Volume 51 Number 5 (Part 2) 1972

The upper limit of k must be k, to correspond to the upper limit of 8=7r/2.

An interesting sidelight is obtained from Eq.

7.

The right-hand side is such that one would expect a constant bounded k spectrum if the correct variables were chosen. If one chooses k,, the wavenumber perpendicular to the surface being considered, then

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T T E R S T O T H E E D 1

a suitable choice of axes we may simplify the B. Incident Field from an Annulus

For this case, we shall take pn(O) = 6(O-Oo) ; i.e., the sound field is restricted to a narrow band of solid angles around Oo, where 6(O-OO) is the impulse function and

6(O-Oo)dO= 1. We may then write

Proceeding as before,

k fk(k) =2n(k/ka2)6(O-O0) (1 -k2/ka2)-f. (9) Similarly, the inverse transform will be given by

[

2 ~ ~ 6 ( O - O ~ ) J ~ ( k r )

(

I--

k:2r'

dk. (10) If in Eq. 8 we put O=2n(l-cose), then

dO= 2" sinode= 2~ sinO(dO/dk)dk and

dk = (dO/2~ sine)ka cost). The correlation function becomes

6(O -Oo) Jo(kr)dO = Jo(kar sineo). (1 1)

C. Two-Dimensional Reverberant Field The equation corresponding to Eq. 4 may be written

p,(e)ae = (1/2,)de (12) and as pe(e)de=+ fk(k)dk. 1

(

- 1

--

ka exp(jkr)dk = Jo(kar). (14)

"

-k, D. Plane-Wave Incidence I n this case, p(e) = s(e-eo) and

Again the inverse transform is given by

ka k2 4

6 - k a (

- )

exp(

11. SUMMARY

Although none of the results for the correlation func- tion for different kinds of spatial distribution is new, the method of analysis has some novelty. When we wish to consider transmission through plates, for example, there is some advantage in expressing the plate impe- dance in terms of k parameters. Then any deviation from the ideally reverberant incident field may be ad- justed by modifying the incident k spectra.

ACKNOWLEDGMENTS

This paper is a contribution from the Division of Building Research, National Research Council of Canada, and is published with the approval of the Director of the Division.

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This publication is being distributed by the Division of Building Research of the National Research Council of Canada. I t should not be reproduced in whole or in part without permission of the original publisher. The Division would be glad to be of assistance in obtaining such permission.

Publications of the Division may be obtained by mailing the appropriate remittance (a Bank, Express, or Post Office Money Order, or a cheque, made payable to the Receiver General of Canada, credit NRC) to the National Research Council of Canada, Ottawa. KIAOR6. Stamps are not acceptable.

A list of all publications of the Division is available and may be obtained from the Publications Section, Division of Building Research, National Research Council of Canada, Ottawa. KIAOR6.

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