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Theoretical studies on tone noise from a ducted fan rotorThe method of computing radiated noise from a ducted rotor due to inflow distortion and turbulence are examined. Analytical investigations include an appropriate description of sources, the cut-off conditions imposed on the modal propagation of the pressure waves in the annular duct, and reflections at the upstream end of the duct. Far field sound pressure levels at blade passing frequency due to acoustic radiation from a small scale low speed fan are computed. Theoretical predictions are in reasonable agreement with experimental measurements.
Document ID
19750006692
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rao, C. V. R.
(Rao and Associates, Inc. Palo Alto, CA, United States)
Chu, W. T.
(Rao and Associates, Inc. Palo Alto, CA, United States)
Digumarthi, R. V.
(Rao and Associates, Inc. Palo Alto, CA, United States)
Agarwal, R. K.
(Rao and Associates, Inc. Palo Alto, CA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1974
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-137620
Report Number: NASA-CR-137620
Accession Number
75N14764
Funding Number(s)
CONTRACT_GRANT: NAS2-6401
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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