Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/111522
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Title: Active control of drag noise from a small axial flow fan
Authors: Wang, J 
Huang, L 
Issue Date: Jul-2006
Source: Journal of the Acoustical Society of America, July 2006, v. 120, no. 1, p. 192-203
Abstract: Noise sources in an axial flow fan can be divided into fluctuating axial thrust forces and circumferential drag forces. For the popular design of a seven-blade rotor driven by a motor supported by four struts, drag noise dominates. This study aims to suppress the drag noise globally by active control schemes. Drag noise features a rotating dipole and it has to be cancelled by a secondary source of the same nature. This is achieved experimentally by a pair of loudspeakers positioned at right angles to each other on the fan rotational plane. An adaptive LMS feedforward scheme is used to produce the control signal for one loudspeaker and the time derivative of this signal is used to drive the other loudspeaker. The antisounds radiated by the two loudspeakers have a fixed phase relation of 90° forming a rotating dipole. An open-loop control scheme is also implemented for the purpose of comparison and easier implementation in real-life applications. The results show that the globally integrated sound power is reduced by about 13 dB for both closed-and open-loop schemes. A possible limiting factor for the cancellation performance is found to be the presence of higher order modes of drag noise.
Publisher: AIP Publishing LLC
Journal: Journal of the Acoustical Society of America 
ISSN: 0001-4966
EISSN: 1520-8524
DOI: 10.1121/1.2204443
Rights: © 2006 Acoustical Society of America. This article may be downloaded for personal use only. Any other use requires prior permission of the author and the Acoustical Society of America.
The following article appeared in Jian Wang, Lixi Huang; Active control of drag noise from a small axial flow fan. J. Acoust. Soc. Am. 1 July 2006; 120 (1): 192–203 and may be found at https://doi.org/10.1121/1.2204443.
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