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Propeller aircraft interior noise modelAn analytical model was developed to predict the interior noise of propeller-driven aircraft. The fuselage model is that of a cylinder with a structurally-integral floor. The cabin sidewall is stiffened by stringers and ring frames, and the floor by longitudinal beams. The cabin interior is covered with a sidewall treatments consisting of layers of porous material and an impervious trim septum. Representation of the propeller pressure field is utilized as input data in the form of the propeller noise signature at a series of locations on a grid over the fuselage structure. Results obtained from the analytical model are compared with test data measured by NASA in a scale model cylindrical fuselage excited by a model propeller.
Document ID
19840021618
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Pope, L. D.
(Bolt, Beranek, and Newman, Inc. Canoga Park, CA, United States)
Wilby, E. G.
(Bolt, Beranek, and Newman, Inc. Canoga Park, CA, United States)
Wilby, J. F.
(Bolt, Beranek, and Newman, Inc. Canoga Park, CA, United States)
Date Acquired
September 4, 2013
Publication Date
July 1, 1984
Subject Category
Acoustics
Report/Patent Number
BBN-5058
NAS 1.26:3813
NASA-CR-3813
Report Number: BBN-5058
Report Number: NAS 1.26:3813
Report Number: NASA-CR-3813
Accession Number
84N29687
Funding Number(s)
CONTRACT_GRANT: NAS1-15782
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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