The Ffowcs Williams and Hawkings (FW-H) equation is widely used to predict sound generated from flow and its interaction with impermeable or permeable surfaces. Owing to the Heaviside function used, this equation assumes that sound only propagates outside the surface. In this paper, we develop a generalized acoustic analogy to account for sound generation and propagation both inside and outside the surface. The developed wave equation provides an efficient mathematical approach to predict sound generated from multiphase or multicomponent flow (MMF) and its interaction with solid boundaries. The developed wave equation also clearly interprets the physical mechanisms of sound generation, emphasizing that the monopole and dipole sources are dependent on the jump in physical quantities across the interface of MMF rather than the physical quantities on one-side surface expressed in the FW-H equation. The sound generated from gas bubbles in water is analyzed by the newly developed wave equation to investigate parameters affecting the acoustic power output, showing that the acoustic power feature concluded from the Crighton and Ffowcs Williams (C-FW) equation is only valid in a specific case of all bubbles oscillating in phase.

References

1.
Lighthill
,
M. J.
,
1952
, “
On Sound Generated Aerodynamically I. General Theory
,”
Proc. R. Soc. London, Ser. A
,
211
(
1107
), pp.
564
587
.
2.
Curle
,
N.
,
1955
, “
The Influence of Solid Boundaries Upon Aerodynamic Sound
,”
Proc. R. Soc. London, Ser. A
,
231
(
1187
), pp.
505
514
.
3.
Ffowcs Williams
,
J.
, and
Hawkings
,
D.
,
1969
, “
Sound Generation by Turbulence and Surfaces in Arbitrary Motion
,”
Philos. Trans. R. Soc., A
,
264
(
1151
), pp.
321
342
.
4.
di Francescantonio
,
P.
,
1997
, “
A New Boundary Integral Formulation for the Prediction of Sound Radiation
,”
J. Sound Vib.
,
202
(
4
), pp.
491
509
.
5.
Brentner
,
K. S.
, and
Farassat
,
F.
,
2003
, “
Modeling Aerodynamically Generated Sound of Helicopter Rotors
,”
Prog. Aerosp. Sci.
,
39
(
2–3
), pp.
83
120
.
6.
Crighton
,
D. G.
, and
Ffowcs Williams
,
J. E.
,
1969
, “
Sound Generation by Turbulent Two-Phase Flow
,”
J. Fluid Mech.
,
36
(
03
), pp.
585
603
.
7.
Howe
,
M. S.
,
1975
, “
Contributions to Theory of Aerodynamic Sound, With Application to Excess Jet Noise and Theory of Flute
,”
J. Fluid Mech.
,
71
(
4
), pp.
625
673
.
8.
Campos
,
L. M. B. C.
,
1978
, “
On the Emission of Sound by an Ionized Inhomogeneity
,”
Proc. R. Soc. London, Ser. A
,
359
(
1696
), pp.
65
91
.
9.
Farassat
,
F.
,
2007
, “
Derivation of Formulations 1 and 1A of Farassat
,” NASA Langley Research Center, Hampton, VA, Report No.
NASA-TM-2007-214853
.https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20070010579.pdf
10.
Ffowcs Williams
,
J. E.
,
1974
, “
Sound Production at the Edge of a Steady Flow
,”
J. Fluid Mech.
,
66
(
4
), pp.
791
816
.
11.
Dowling
,
A. P.
,
Williams
,
J. E. F.
, and
Goldstein
,
M. E.
,
1978
, “
Sound Production in a Moving Stream
,”
Philos. Trans. R. Soc., A
,
288
(
1353
), pp.
321
349
.
12.
Tang
,
H. T.
,
Qi
,
D. T.
, and
Mao
,
Y. J.
,
2013
, “
Analysis on the Frequency-Domain Numerical Method to Compute the Noise Radiated From Rotating Sources
,”
J. Sound Vib.
,
332
(
23
), pp.
6093
6103
.
13.
Mao
,
Y. J.
,
Gu
,
Y. Y.
,
Qi
,
D. T.
, and
Tang
,
H. T.
,
2012
, “
An Exact Frequency-Domain Solution of the Sound Radiated From the Rotating Dipole Point Source
,”
J. Acoust. Soc. Am.
,
132
(
3
), pp.
1294
1302
.
14.
Mao
,
Y. J.
,
Xu
,
C.
,
Qi
,
D. T.
, and
Tang
,
H. T.
,
2014
, “
Series Expansion Solution for Sound Radiation From Rotating Quadrupole Point Source
,”
AIAA J.
,
52
(
5
), pp.
1086
1095
.
15.
Wells
, V
. L.
, and
Han
,
A. Y.
,
1995
, “
Acoustics of a Moving Source in a Moving Medium With Application to Propeller Noise
,”
J. Sound Vib.
,
184
(
4
), pp.
651
663
.
16.
Najafi-Yazdi
,
A.
,
Bres
,
G. A.
, and
Mongeau
,
L.
,
2011
, “
An Acoustic Analogy Formulation for Moving Sources in Uniformly Moving Media
,”
Proc. R. Soc. London, Ser. A
,
467
(
2125
), pp.
144
165
.
17.
Ghorbaniasl
,
G.
, and
Lacor
,
C.
,
2012
, “
A Moving Medium Formulation for Prediction of Propeller Noise at Incidence
,”
J. Sound Vib.
,
331
(
1
), pp.
117
137
.
18.
Howe
,
M. S.
,
1975
, “
Generation of Sound by Aerodynamic Sources in an Inhomogeneous Steady Flow
,”
J. Fluid Mech.
,
67
(
3
), pp.
597
610
.
19.
Howe
,
M. S.
,
1998
,
Acoustics of Fluid–Structure Interaction
,
Cambridge University Press
,
Cambridge, UK
.
You do not currently have access to this content.