THE ABSORPTION OF SOUND NEAR ABRUPT AXISYMMETRIC AREA EXPANSIONS

Abstract Sound incident onto an abrupt area expansion in an axisymmetric pipe is investigated analytically and experimentally. The incident sound field may synchronize the unsteady shedding of vorticity at the lip of the expansion to produce an organized train of vortices. In the presence of a mean flow, the unsteady vorticity shed from the lip is convected downstream where it acts as a sink or source of sound, thereby converting acoustic into vortical energy, or vice versa. An acoustic analogy and a Green function, G, are used to determine the sound reflected and transmitted across the area change. One finds that there is an optimal Strouhal number at which sound absorption is maximized and that this absorption can be enhanced by multiple reflections from the duct ends. In addition, the appropriate distance to be used in the definition of the Strouhal number depends upon the diameter ratio of the pipe expansion, λ=a/b, where a is the radius of the small pipe, and b is the radius of the larger pipe. For small λ, the appropriate length scale is the pipe radius, a; whereas for λ nearly equal to unity the appropriate length scale is the step height b−a. Predictions are compared with experiment.

[1]  Sw Sjoerd Rienstra,et al.  On the acoustical implications of vortex shedding from an exhaust pipe , 1980 .

[2]  M. Lighthill On sound generated aerodynamically II. Turbulence as a source of sound , 1954, Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences.

[3]  P. Nelson,et al.  Fluid dynamics of a flow excited resonance, Part II: Flow acoustic interaction , 1983 .

[4]  Irene A. Stegun,et al.  Handbook of Mathematical Functions. , 1966 .

[5]  A. F. Seybert,et al.  Experimental determination of acoustic properties using a two‐microphone random‐excitation technique , 1977 .

[6]  Ann P. Dowling,et al.  Absorption of Sound near Abrupt Area Expansions , 2000 .

[7]  M. S. Howe,et al.  On the theory of unsteady high Reynolds number flow through a circular aperture , 1979, Proceedings of the Royal Society of London. A. Mathematical and Physical Sciences.

[8]  R. Munt The interaction of sound with a subsonic jet issuing from a semi-infinite cylindrical pipe , 1977, Journal of Fluid Mechanics.

[9]  Yasuhide Fukumoto,et al.  Vorticity production at the edge of a slit by sound waves in the presence of a low-mach-number bias flow , 1991 .

[10]  C. L. Morfey,et al.  Sound transmission and generation in ducts with flow , 1971 .

[11]  A. F. Seybert,et al.  Error analysis of spectral estimates with application to the measurement of acoustic parameters using random sound fields in ducts , 1981 .

[12]  A. Powell Theory of Vortex Sound , 1964 .

[13]  M. Lighthill On sound generated aerodynamically I. General theory , 1952, Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences.

[14]  J. Schwinger,et al.  On the Radiation of Sound from an Unflanged Circular Pipe , 1948 .

[15]  M. S. Howe The influence of vortex shedding on the diffraction of sound by a perforated screen , 1980, Journal of Fluid Mechanics.

[16]  G. F. Carrier Sound transmission from a tube with flow , 1956 .

[17]  U. Ingard,et al.  Acoustic Circulation Effects and the Nonlinear Impedance of Orifices , 1950 .

[18]  R. Munt,et al.  Acoustic transmission properties of a jet pipe with subsonic jet flow: I. The cold jet reflection coefficient , 1990 .

[19]  A Avraham Hirschberg,et al.  Damping and reflection coefficient measurements for an open pipe at low Mach and low Helmholtz numbers , 1993, Journal of Fluid Mechanics.

[20]  Ann P. Dowling,et al.  Sound absorption by a screen with a regular array of slits , 1992 .

[21]  A. M. Cargill,et al.  Low-frequency sound radiation and generation due to the interaction of unsteady flow with a jet pipe , 1982, Journal of Fluid Mechanics.

[22]  Michael S. Howe,et al.  Attenuation of sound in a low Mach Number nozzle flow , 1979, Journal of Fluid Mechanics.

[23]  Sw Sjoerd Rienstra,et al.  A small strouhal number analysis for acoustic wave - jet flow - pipe interaction , 1980 .

[24]  H. Levin On the radiation of sound from an unflanged circular pipe , 1948 .

[25]  M. S. Howe Contributions to the theory of aerodynamic sound, with application to excess jet noise and the theory of the flute , 1975, Journal of Fluid Mechanics.

[26]  M. S. Howe On the diffraction of sound by a screen with circular apertures in the presence of a low Mach number grazing flow , 1980, Proceedings of the Royal Society of London. A. Mathematical and Physical Sciences.

[27]  A. M. Cargill,et al.  Low frequency acoustic radiation from a jet pipe—a second order theory , 1982 .

[28]  E. Pfizenmaier,et al.  Experiments on the Transmission of Sound Through Jets , 1977 .

[29]  D. W. Bechert,et al.  Sound absorption caused by vorticity shedding, demonstrated with a jet flow☆ , 1980 .

[30]  P.O.A.L. Davies,et al.  Reflection coefficients for an unflanged pipe with flow , 1980 .

[31]  A. Dowling,et al.  The absorption of sound by perforated linings , 1990, Journal of Fluid Mechanics.

[32]  D. Crighton The Kutta Condition in Unsteady Flow , 1985 .

[33]  P. Doak Momentum potential theory of energy flux carried by momentum fluctuations , 1989 .

[34]  Istvan L. Ver Practical Examples of Noise and Vibration Control: Case History of Consulting Projects , 1990 .

[35]  S. D. Savkar,et al.  Radiation of cylindrical duct acoustic modes with flow mismatch. [effects on aircraft engine noise] , 1975 .

[36]  P. G. Daniels,et al.  ON THE UNSTEADY KUTTA CONDITION , 1978 .

[37]  P. E. Doak,et al.  Fluctuating Total Enthalpy as the Basic Generalized Acoustic Field , 1998 .

[38]  P. Nelson,et al.  Fluid dynamics of a flow excited resonance, part I: Experiment , 1981 .

[39]  A. Cummings Acoustic nonlinearities and power losses at orifices , 1984 .

[40]  U. Ingard,et al.  Acoustic Nonlinearity of an Orifice , 1967 .