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Acoustic Aspects of Active-Twist Rotor ControlThe use of an Active Twist Rotor system to provide both vibration reduction and performance enhancement has been explored in recent analytical and experimental studies. Effects of active-twist control on rotor noise, however, had not been determined. During a recent wind tunnel test of an active-twist rotor system, a set of acoustic measurements were obtained to assess the effects of active-twist control on noise produced by the rotor, especially blade-vortex interaction (BVI) noise. It was found that for rotor operating conditions where BVI noise is dominant, active-twist control provided a reduction in BVI noise level. This BVI noise reduction was almost, but not quite, as large as that obtained in a similar test using HHC. However, vibration levels were usually adversely affected at operating conditions favoring minimum BVI noise. Conversely, operating conditions favoring minimum vibration levels affected BVI noise levels, but not always adversely.
Document ID
20030015483
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Booth, Earl R., Jr.
(NASA Langley Research Center Hampton, VA United States)
Wilbur, Matthew L.
(Army Research Lab. Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Acoustics
Meeting Information
Meeting: American Helicopter Society 58th Annual Forum
Location: Montreal
Country: Canada
Start Date: June 11, 2002
End Date: June 13, 2002
Sponsors: American Helicopter Society, Inc.
Distribution Limits
Public
Copyright
Public Use Permitted.
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