Sound source localization of flow around circular cylinder by a virtual microphone array technique
Source abstract
Abstract
Sound source localization technology is used to study the noise mechanism generated by flow around a circular cylinder. Detached-eddy simulation is performed to compute the flow field and the far-field noise is calculated with the Ffowcs Williams and Hawkings acoustic analogy. At first the simulation method is validated with the flow around circular cylinder at Re=3900. The numerical results are compared with the experimental data by other researchers. The following case is to simulate the flow around circular cylinder at Re=46000. The acoustic result is found in good agreement with the experimental measurements. The acoustic analogy result is used as an input for the noise localization process. Microphone array technique is applied to investigate sound generated by flow around a circular cylinder with emphasis on sound generation mechanism. Two sound source localization methods are considered, including Delay-and-Sum beamforming algorithm and a high resolution beamforming method. The sound source is associated with the lift dipole at the vortex shedding frequency. The sound source is associated with the drag dipole at the double vortex shedding frequency. The sound source can also be shown at other frequency. With frequency increasing, the strength reduces and there are some other sidelobe sources.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Fluid Dynamics and Vibration Analysis · Aerodynamics and Acoustics in Jet Flows · Wind and Air Flow Studies
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
School of Energy and Power Engineering, Beihang University , Beijing 100083, China
References (29)
Show source-provided references
1. Vortex dynamics in the cylinder wake10.1146/annurev.fl.28.010196.002401 ↗
2. The influence of solid boundaries upon aerodynamic sound10.1098/rspa.1955.0191 ↗
3. The intensity of aeolian tones10.1017/s0022112056000408 ↗
4. Acoustic radiation from a stationary cylinder in a finite stream (aeolian tones)10.1121/1.1908673 ↗
5. Measurements of the sound from circular cylinders in an air stream10.1088/0370-1301/68/7/307 ↗
6. Sound generation by a two-dimension circular cylinder in a uniform flow10.1017/s0022112002002124 ↗
7. Comments on the feasibility of LES for wings, and on a hybrid RANS/LES approach
8. Detached-eddy simulation10.1146/annurev.fluid.010908.165130 ↗
9. J. Cox, C. Rumsey, K. Brentner, and B. Younis, “Computation of sound generated by viscous flow over a circular cylinder,” Tech. Rep. TM 110339, NASA (1997).10.1115/IMECE1997-0088 ↗
10. 2002
11. Phased arrays for aeroacoustic testing-theoretical development
12. Sidelobe suppression for phased array aeroacoustic measurements
13. A deconvolution approach for the mapping of acoustic sources (DAMAS) determined from phased microphone arrays
14. CLEAN based on spatial source coherence
15. Localization of airfoil self-noise sources by a virtual phased microphone array technique
16. Sound source localization via elastic net regularization
17. Identification and localization of airfoil noise sources at low angles of attack
18. Characteristics of the plane turbulent near wake of a circular cylinder, a particle image velocity study
19. Experimental and numerical studies of flow over a circular cylinder at Reynolds number 390010.1063/1.2957018 ↗
20. An experimental investigation of flow around a circular cylinder: Influence of aspect ratio
21. Sound generated by turbulence and surface in arbitrary motion10.1098/rsta.1969.0031 ↗
22. Linear acoustic formulas for calculation of rotating blade noise10.2514/3.60051 ↗
23. Numerical studies of flow over a circular cylinder at Re=390010.1063/1.870318 ↗
24. A combined direct numerical simulation particle image velocity study of the turbulent near wake10.1017/s0022112006002606 ↗
25. Dynamics and low-dimensionality of turbulent near wake10.1017/s0022112099007934 ↗
26. Large eddy simulation of the flow past a circular cylinder at Re=390010.1016/s0167-6105(02)00232-5 ↗
27. Prediction of sound radiated by a rod using large eddy simulation
28. Aerodynamic noise prediction for long-span bodies10.1016/j.jsv.2007.05.042 ↗
29. Toward hybrid CAA with ground effects10.1260/1475-472x.13.3-4.235 ↗