Fast Low-Storage Method for Evaluating Lighthill's Volume Quadrupoles

An m-multipole particle-condensation method is proposed to spatially condense the volumetric quadrupole sources based on Lighthill’s acoustic analogy that are extracted from computational-fluid-dynamics data. The purpose of the method is to reduce both the amount of data that must be stored during the computational-fluid-dynamics analysis and the number of acoustic sources driving the subsequent acoustic-propagation analysis, while preserving the accuracy of the predicted sound pressure field. The method uses a particle approximation of the quadrupole source distribution and employs a Taylor series expansion of the harmonic Green’s function to spatially condense the underlying acoustic sources and preserve their multipole moments. Low-Mach-number flow around rigid-walled stationary bodies in a medium at rest at infinity is used to demonstrate the m-multipole particle-condensation method. The directivity of the sound pressure field due to the quadrupole sources is presented for the first four harmonics of ...

[1]  Parviz Moin,et al.  Prediction of Sound Generated by Complex Flows at Low Mach Numbers , 2010 .

[2]  D. Casalino An advanced time approach for acoustic analogy predictions , 2003 .

[3]  P. D. Francescantonio A NEW BOUNDARY INTEGRAL FORMULATION FOR THE PREDICTION OF SOUND RADIATION , 1997 .

[4]  D. L. Hawkings,et al.  Sound generation by turbulence and surfaces in arbitrary motion , 1969, Philosophical Transactions of the Royal Society of London. Series A, Mathematical and Physical Sciences.

[5]  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.

[6]  Meng Wang,et al.  LES Prediction of Wall-Pressure Fluctuations and Noise of a Low-Speed Airfoil , 2009 .

[7]  S. Marburg SIX BOUNDARY ELEMENTS PER WAVELENGTH: IS THAT ENOUGH? , 2002 .

[8]  T. Poinsot Boundary conditions for direct simulations of compressible viscous flows , 1992 .

[9]  Siegfried Wagner,et al.  Source-time dominant aeroacoustics , 2004 .

[10]  S. Orszag,et al.  Approximation of radiation boundary conditions , 1981 .

[11]  C. Bailly,et al.  Flow-induced cylinder noise formulated as a diffraction problem for low Mach numbers , 2005 .

[12]  C. Schram,et al.  Correction techniques for the truncation of the source field in acoustic analogies. , 2008, The Journal of the Acoustical Society of America.

[13]  Francois Vuillot,et al.  Theoretical and Numerical Discussion on Volume Integral Methods for Jet Noise Prediction , 2007 .

[14]  I. Orlanski A Simple Boundary Condition for Unbounded Hyperbolic Flows , 1976 .

[15]  Uwe Fey,et al.  A new Strouhal–Reynolds-number relationship for the circular cylinder in the range 47 , 1998 .

[16]  S. Marburg,et al.  INFLUENCE OF ELEMENT TYPES ON NUMERIC ERROR FOR ACOUSTIC BOUNDARY ELEMENTS , 2003 .

[17]  T. Hughes,et al.  Computational procedures for determining structural-acoustic response due to hydrodynamic sources , 2000 .

[18]  Stefan Becker,et al.  Numerical simulation of flow‐induced noise using LES/SAS and Lighthill's acoustic analogy , 2009 .

[19]  J. Freund A Simple Method for Computing Far-Field Sound in Aeroacoustic Computations , 2000 .

[20]  Sanjiva K. Lele,et al.  Acoustic Analogy Formulations Accelerated by Fast Multipole Method for Two-Dimensional Aeroacoustic Problems , 2010 .

[21]  O. Posdziech,et al.  A systematic approach to the numerical calculation of fundamental quantities of the two-dimensional flow over a circular cylinder , 2007 .

[22]  N. Curle The influence of solid boundaries upon aerodynamic sound , 1955, Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences.

[23]  Stéphane Caro,et al.  Validation of a New Hybrid CAA Strategy and Application to the Noise Generated by a Flap in a Simplified HVAC Duct , 2009 .

[24]  Ramani Duraiswami,et al.  A broadband fast multipole accelerated boundary element method for the three dimensional Helmholtz equation. , 2009, The Journal of the Acoustical Society of America.

[25]  C. Norberg Flow around a Circular Cylinder: Aspects of Fluctuating Lift , 2001 .

[26]  J. Williams,et al.  Aerodynamic sound generation by turbulent flow in the vicinity of a scattering half plane , 1970, Journal of Fluid Mechanics.

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

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