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En route noise of two turboprop aircraftIn order to weigh en route noise emissions originating from future propfan powered aircraft, a data base of emission levels from conventional turboprop aircraft is needed. For this reason flyover noise measurements on two twin-engine turboprop aircraft were conducted at flight heights between 17,000 and 21,000 ft. Acoustic data are presented together with propeller operational parameters and environmental meteorological data. Narrowband spectral analyses demonstrate the characteristic features of the measured propeller noise signatures: Noise spectra are dominated by the propeller rotational noise fundamental frequency and pronounced noise beats occur as a consequence of different rotational speeds of the propellers.
Document ID
19900015543
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dobrzynski, Werner
(Deutsche Forschungsanstalt fuer Luft- und Raumfahrt Brunswick, Germany)
Date Acquired
September 6, 2013
Publication Date
April 1, 1990
Publication Information
Publication: NASA, Langley Research Center, FAA(NASA En Route Noise Symposium
Subject Category
Acoustics
Report/Patent Number
DLR-MITT-89-18
Report Number: DLR-MITT-89-18
Accession Number
90N24859
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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