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Interior noise reduction in a large civil helicopterThe results of an evaluation of the effectiveness of current noise reduction technology in attaining acceptable levels of interior noise in a large (about 20,000 kg) passenger-carrying helicopter are presented. The helicopter studied is a modified CH-53A with a specially designed, acoustically treated passenger cabin. The acoustic treatment reduced the average A-weighted interior noise levels from 115 db to 87 db. The study suggests selected improvements in the acoustic treatment which could result in additional reduction in cabin noise levels. The resulting levels would be only slightly greater than the interior noise levels of current narrow-body jet transports.
Document ID
19770021967
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Howlett, J. T.
(NASA Langley Research Center Hampton, VA, United States)
Clevenson, S. A.
(NASA Langley Research Center Hampton, VA, United States)
Rypf, J. A.
(Joint Inst. for Advan. of Flight Sci. Hampton, Va., United States)
Snyder, W. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1977
Subject Category
Acoustics
Report/Patent Number
NASA-TN-D-8477
L-11349
Accession Number
77N28911
Funding Number(s)
PROJECT: RTOP 505-10-26-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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