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Noise reduction studies of several aircraft to reduce their aural detection distancesA study was conducted to assess the extent to which practicable reductions of the external noise level of various aircraft could be achieved by different methods. The aircraft included in the study are the O-1, O-2, U-10, OV-1, and A-6. The noise signatures obtained from field measurements and the estimated aural detection distance of aircraft operating in low speed cruising flight are presented. The characteristics of each aircraft and the modifications made to reduce the aerodynamic noise are explained. Tables of data are included to show the effectiveness of the noise reduction modifications for each aircraft.
Document ID
19750010163
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Dingeldein, R. C.
(NASA Langley Research Center Hampton, VA, United States)
Connor, A. B.
(NASA Langley Research Center Hampton, VA, United States)
Hilton, D. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1975
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-X-72644
Report Number: NASA-TM-X-72644
Accession Number
75N18235
Funding Number(s)
PROJECT: RTOP 505-03-12-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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