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Interior noise levels of two propeller-driven light aircraftThe relationships between aircraft operating conditions and interior noise and the degree to which ground testing can be used in lieu of flight testing for performing interior noise research were studied. The results show that the noise inside light aircraft is strongly influenced by the rotational speed of the engine and propeller. Both the overall noise and low frequency spectra levels were observed to decrease with increasing high speed rpm operations during flight. This phenomenon and its significance is not presently understood. Comparison of spectra obtained in flight with spectra obtained on the ground suggests that identification of frequency components and relative amplitude of propeller and engine noise sources may be evaluated on stationary aircraft.
Document ID
19750019994
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Catherines, J. J.
(NASA Langley Research Center Hampton, VA, United States)
Mayes, W. H.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1975
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-X-72716
Report Number: NASA-TM-X-72716
Accession Number
75N28066
Funding Number(s)
PROJECT: RTOP 504-09-21-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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