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Rotor noise prediction technology: Theoretical approachHelicopter rotors which are the most complicated noise generators among rotating blade machinery are discussed. The main or the tail rotor can be the dominant source of noise depending on the range of frequencies and the observer position. Significant advances in noise prediction were made. Acoustic analysis is the most successful and general theoretical method to treat the acoustics of helicopter noise. The aerodynamic approach is used to study nonlinear acoustic effects. The results of acoustic analogy depend greatly on the input data.
Document ID
19840021609
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Farassat, F.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
July 1, 1982
Publication Information
Publication: Rotorcraft Noise
Subject Category
Acoustics
Accession Number
84N29678
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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