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General aviation aircraft interior noise problem: Some suggested solutionsLaboratory investigation of sound transmission through panels and the use of modern data analysis techniques applied to actual aircraft is used to determine methods to reduce general aviation interior noise. The experimental noise reduction characteristics of stiffened flat and curved panels with damping treatment are discussed. The experimental results of double-wall panels used in the general aviation industry are given. The effects of skin panel material, fiberglass insulation and trim panel material on the noise reduction characteristics of double-wall panels are investigated. With few modifications, the classical sound transmission theory can be used to design the interior noise control treatment of aircraft. Acoustic intensity and analysis procedures are included.
Document ID
19840021616
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Roskam, J.
(Kansas Univ. Lawrence, KS, United States)
Navaneethan, R.
(Kansas Univ. Lawrence, KS, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1984
Subject Category
Acoustics
Report/Patent Number
NAS 1.26:173784
KU-FRL-417-23
NASA-CR-173784
Report Number: NAS 1.26:173784
Report Number: KU-FRL-417-23
Report Number: NASA-CR-173784
Accession Number
84N29685
Funding Number(s)
CONTRACT_GRANT: NCC1-6
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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