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Flow noise from spoilers in ducts

J. Acoust. Soc. Am. Volume 125, Issue 6, pp. 3756-3765 (2009); (10 pages)

Cheuk Ming Mak1, Jia Wu1, Chao Ye2, and Jun Yang3

1Department of Building Services Engineering, The Hong Kong Polytechnic University, Hung Hom, Kowloon, Hong Kong, China
2Department of Building Services Engineering, The Hong Kong Polytechnic University, Hung Hom, Kowloon, Hong Kong, China and State Key Laboratory of Acoustics, Institute of Acoustics, Chinese Academy of Sciences, Beijing 100080, China
3State Key Laboratory of Acoustics, Institute of Acoustics, Chinese Academy of Sciences, Beijing 100080, China

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Measurements of flow noise produced by strip spoilers in the air duct of a ventilation system and radiated from an open exhaust termination unit into a reverberation chamber have been made. The results agree with the previous work of Nelson and Morfey [J. Sound Vib. 79, 263–289 (1981)] . Prediction of flow noise produced by multiple spoilers requires the values of the ratio of the mean drag forces that act on the spoilers, the phase relationship between the fluctuating drag forces that act on the spoilers, and the coherence function of the noise sources. The latter is empirically derived from the measured results, where the predicted results agree well with the experimental results within 3 dB at most frequencies except for very high frequencies.

© 2009 Acoustical Society of America

ACKNOWLEDGMENTS

The work described in this paper was fully supported by a grant from the Research Grants Council of the Hong Kong Special Administrative Region, China (Project No. PolyU 5229/05E).

Article Outline

  1. INTRODUCTION
  2. THEORY AND PREDICTIVE EQUATIONS OF NOISE PRODUCED BY IN-DUCT FLOW SPOILER(S)
  3. EXPERIMENTAL PROCEDURE
    1. Design of the experimental rig
    2. The spoilers used in the experiment
    3. Airflow measurements
    4. Acoustic measurements
    5. Force measurements
  4. ANALYSIS AND DISCUSSION OF THE RESULTS
    1. Normalization of the experimental results for a single flow spoiler
    2. Determination of the coherence function of noise sources
    3. Comparison between predicted and measured results
  5. CONCLUSION

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KEYWORDS and PACS

PACS

  • 43.50.Nm

    Aerodynamic and jet noise

  • 43.50.Ed

    Noise generation

  • 43.50.Cb

    Noise spectra, determination of sound power

  • 43.28.Ra

    Generation of sound by fluid flow, aerodynamic sound and turbulence

ARTICLE DATA

History
Received 17 Apr 2008
Accepted 10 Apr 2009
Revised 28 Mar 2009

PUBLICATION DATA

ISSN

0001-4966 (print)  

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