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Preliminary experiments on active control of fan noise from a turbofan engineIn the preliminary experiments reported here, active acoustic sources positioned around the circumference of a turbofan engine were used to control the fan noise radiated forward through the inlet. The main objective was to demonstrate the potential of active techniques to alleviate the noise pollution that will be produced by the next generation of larger engines. A reduction of up to 19 dB in the radiation directivity was demonstrated in a zone that encompasses a 30-deg angle, near the error sensor, while spillover effects were observed toward the lateral direction. The simultaneous control of two tones was also demonstrated using two identical controllers in a parallel control configuration.
Document ID
19930050960
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Thomas, R. H.
(NASA Langley Research Center Hampton, VA, United States)
Burdisso, R. A.
(NASA Langley Research Center Hampton, VA, United States)
Fuller, C. R.
(NASA Langley Research Center Hampton, VA, United States)
O'Brien, W. F.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, United States)
Date Acquired
August 16, 2013
Publication Date
March 8, 1993
Publication Information
Publication: Journal of Sound and Vibration
Volume: 161
Issue: 3
ISSN: 0022-460X
Subject Category
Acoustics
Accession Number
93A34957
Funding Number(s)
CONTRACT_GRANT: NAS1-18471
Distribution Limits
Public
Copyright
Other

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