Application of an acoustic analogy to PIV data from rectangular cavity flows

The present paper describes a method to derive information about the acoustic emission of a flow using particle image velocimetry (PIV) data. The advantage of the method is that it allows studying sound sources, the related flow phenomena and their acoustic radiation into the far field, simultaneously. In a first step the time history of two-dimensional instantaneous pressure fields is derived from planar PIV data. In a successive step the Curle’s acoustic analogy is applied to the pressure data to obtain the acoustic radiation of the flow. The test cases studied here are two rectangular cavity flows at very low Mach number with different aspect ratios L/H. The main sound source is located at the cavity trailing edge and it is due to the impingement of vortices shed in the shear layer. It is shown that the flow emits sound with a main directivity in the upstream direction for the smaller aspect ratio and the directivity is more uniform for the larger aspect ratio. In the latter case the acoustic pressure spectra has a broader character due to the impact of the downstream recirculation zone onto the shear layer instabilities, destroying their regular pattern and alternating the main sound source.

[1]  Sheryl M. Grace,et al.  Experimental investigation of the flow characteristics within a shallow wall cavity for both laminar and turbulent upstream boundary layers , 2004 .

[2]  K. K. Ahuja,et al.  Prediction and measurement of flows over cavities - A survey , 1987 .

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

[4]  Christopher K. W. Tam,et al.  Computational Aeroacoustics: An Overview of Computational Challenges and Applications , 2004 .

[5]  F. Scarano,et al.  Experimental assessment of Tomographic-PIV accuracy , 2006 .

[6]  M. Y. Hussaini,et al.  COMPUTATION OF THE ACOUSTIC RADIATION FROM BOUNDED HOMOGENEOUS FLOWS , 1993 .

[7]  J. Rossiter Wind tunnel experiments on the flow over rectangular cavities at subsonic and transonic speeds , 1964 .

[8]  C. Tam,et al.  On the tones and pressure oscillations induced by flow over rectangular cavities , 1978, Journal of Fluid Mechanics.

[9]  S. Balachandar,et al.  Mechanisms for generating coherent packets of hairpin vortices in channel flow , 1999, Journal of Fluid Mechanics.

[10]  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.

[11]  Xavier Gloerfelt,et al.  Calcul direct du rayonnement acoustique d'un écoulement affleurant une cavité , 2000 .

[12]  Lars-Erik Eriksson,et al.  Aeroacoustic Investigation of an Open Cavity at Low Mach Number , 2004 .

[13]  Kenji Takeda,et al.  Cavity Tones by Computational Aeroacoustics , 2004 .

[14]  K. K. Ahuja,et al.  Effects of cavity dimensions, boundary layer, and temperature on cavity noise with emphasis on benchmark data to validate computational aeroacoustic codes , 1995 .

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

[16]  Yves Gervais,et al.  Theoretical and experimental investigations of low Mach number turbulent cavity flows , 2004 .

[17]  C. Rowley,et al.  On self-sustained oscillations in two-dimensional compressible flow over rectangular cavities , 2002, Journal of Fluid Mechanics.

[18]  Joseph Katz,et al.  Instantaneous pressure and material acceleration measurements using a four-exposure PIV system , 2006 .

[19]  A. Lyrintzis Review: the use of Kirchhoff's method in computational aeroacoustics , 1994 .

[20]  C. Rowley,et al.  Numerical investigation of the flow past a cavity , 1999 .

[21]  Bernhard Wieneke,et al.  Tomographic particle image velocimetry , 2006 .

[22]  Atle Jensen,et al.  Optimization of acceleration measurements using PIV , 2004 .

[23]  W. Southwell Wave-front estimation from wave-front slope measurements , 1980 .

[24]  Clarence W. Rowley,et al.  Dynamics and control of high-reynolds-number flow over open cavities , 2006 .

[25]  Fulvio Scarano,et al.  Investigation of the flow in a rectangular cavity using tomographic and time-resolved PIV , 2007 .

[26]  T. Colonius,et al.  Computational aeroacoustics: progress on nonlinear problems of sound generation , 2004 .

[27]  William H. Press,et al.  Numerical recipes in C , 2002 .

[28]  Xavier Gloerfelt,et al.  Direct computation of the noise radiated by a subsonic cavity flow and application of integral methods , 2003 .

[29]  D. Rockwell,et al.  Review—Self-Sustaining Oscillations of Flow Past Cavities , 1978 .

[30]  Morteza Gharib,et al.  The effect of flow oscillations on cavity drag , 1987, Journal of Fluid Mechanics.

[31]  Xavier Gloerfelt,et al.  Aerodynamic Noise Induced by Laminar and Turbulent Boundary Layers over Rectangular Cavities , 2002 .

[32]  C. M. Shieh,et al.  Parallel Numerical Simulation of Subsonic Cavity Noise , 1999 .

[33]  J. Herrmann,et al.  Least-squares wave front errors of minimum norm , 1980 .

[34]  Alan Powell,et al.  On the Edgetone , 1961 .

[35]  Aldo Rona,et al.  The Acoustic Resonance of Rectangular and Cylindrical Cavities , 2007 .

[36]  V. Sarohia Experimental investigation of oscillations in flows over shallow cavities , 1976 .