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A summary and evaluation of semi-empirical methods for the prediction of helicopter rotor noiseExisting prediction techniques are compiled and described. The descriptions include input and output parameter lists, required equations and graphs, and the range of validity for each part of the prediction procedures. Examples are provided illustrating the analysis procedure and the degree of agreement with experimental results.
Document ID
19800007615
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Pegg, R. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1979
Subject Category
Acoustics
Report/Patent Number
NASA-TM-80200
Report Number: NASA-TM-80200
Accession Number
80N15875
Funding Number(s)
PROJECT: RTOP 505-42-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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