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Propfan noise propagationThe unconventional supersonic tip speed of advanced propellers has led to uncertainties about Propfan's noise acceptability and compliance with Federal Aviation Noise Regulation (FAR 36). Overhead flight testing of the Propfan with an SR-7L blade during 1989's Propfan Test Assessment (PTA) Program have shown unexpectedly high far-field sound pressure levels. This study here attempts to provide insights into the acoustics of a single-rotating propeller (SRP) with supersonic tip speed. At the same time, the role of the atmosphere in shaping the far-field noise characteristics is investigated.
Document ID
19930010699
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
George, Albert R.
(Cornell Univ. Ithaca, NY, United States)
Sim, Ben WEL-C.
(Cornell Univ. Ithaca, NY, United States)
Date Acquired
September 6, 2013
Publication Date
February 15, 1993
Subject Category
Acoustics
Report/Patent Number
NAS 1.26:192221
NASA-CR-192221
Report Number: NAS 1.26:192221
Report Number: NASA-CR-192221
Accession Number
93N19888
Funding Number(s)
CONTRACT_GRANT: NAG1-1078
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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