SIMILARITY VARIABLES FOR SOUND RADIATION IN A UNIFORM FLOW

Abstract This paper derives a parametric family of similarity variables for describing sound radiation in a uniform flow. The variables, based on a Lorentz-type transformation between the wave equation and the convected wave equation, contain Doppler factors and generalize the Prandtl–Glauert variables used in aerodynamics. The parameter specifying the family may be chosen to match the frequency dependence of the sound on the Mach number of the flow in problem being solved. The variables are used to derive a “fundamental rule” for obtaining a solution of the convected wave equation from a solution of the unconvected wave equation; the rule does not correspond to a Galilean transformation. The method of the paper is applied to several examples from aeroacoustics, including a thickness-noise acoustic source modelled by the Ffowcs Williams–Hawkings equation; a point-force acoustic source; a spatially extended time-harmonic source; a duct mode; and the sound radiated during blade–vortex interaction.

[1]  S. Chu,et al.  Prediction of Unsteady Airloads for Oblique Blade-Gust Interaction in Compressible Flow , 1974 .

[2]  J. Graham,et al.  Similarity rules for thin aerofoils in non-stationary subsonic flows , 1970, Journal of Fluid Mechanics.

[3]  R. Amiet GUST RESPONSE OF A FLAT-PLATE AEROFOIL IN THE TIME DOMAIN , 1986 .

[4]  The effect of flow on the piston problem of acoustics , 1979 .

[5]  F. G. Leppington,et al.  Modern Methods in Analytical Acoustics , 1992 .

[6]  Valana Wells,et al.  Acoustics of a moving source in a moving medium with application to propeller noise , 1995 .

[7]  P. Nelson,et al.  Active control of source sound power radiation in uniform flow , 1998 .

[8]  I. E. Garrick,et al.  A theoretical study of the effect of forward speed on the free-space sound-pressure field around propellers , 1953 .

[9]  C. J. Chapman Sound radiation from a cylindrical duct. Part 2. Source modelling, nil-shielding directions, and the open-to-ducted transfer function , 1996 .

[10]  K. Taylor,et al.  Acoustic generation by vibrating bodies in homentropic potential flow at low Mach number , 1979 .

[11]  Ann P. Dowling,et al.  CONVECTIVE AMPLIFICATION OF REAL SIMPLE SOURCES , 1976 .

[12]  K. Taylor A transformation of the acoustic equation with implications for wind-tunnel and low-speed flight tests , 1978, Proceedings of the Royal Society of London. A. Mathematical and Physical Sciences.

[13]  Sheila E. Widnall,et al.  Unified aerodynamic-acoustic theory for a thin rectangular wing encountering a gust , 1980 .

[14]  John W. Miles,et al.  The Potential Theory of Unsteady Supersonic Flow , 1959 .

[15]  D. Crighton,et al.  An asymptotic theory of near-field propeller acoustics , 1991, Journal of Fluid Mechanics.

[16]  Sheila E. Widnall,et al.  An aeroacoustic model for high-speed, unsteady blade-vortex interaction , 1983 .