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Acoustical analysis of gear housing vibrationThe modal and acoustical analysis of the NASA gear-noise rig is described. Experimental modal analysis techniques were used to determine the modes of vibration of the transmission housing. The resulting modal data were then used in a boundary element method (BEM) analysis to calculate the sound pressure and sound intensity on the surface of the housing as well as the radiation efficiency of each mode. The radiation efficiencies of the transmission housing modes are compared with theoretical results for finite, baffled plates. A method that uses the measured mode shapes and the BEM to predict the effect of simple structural changes on the sound radiation efficiency of the modes of vibration is also described.
Document ID
19930045423
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Seybert, A. F.
(NASA Lewis Research Center Cleveland, OH, United States)
Wu, T. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Wu, X. F.
(Kentucky Univ. Lexington, United States)
Oswald, Fred B.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1991
Publication Information
Publication: In: AHS and Royal Aeronautical Society, Technical Specialists' Meeting on Rotorcraft Acoustics(Fluid Dynamics, Philadelphia, PA, Oct. 15-17, 1991, Proceedings (A93-29401 10-71)
Publisher: American Helicopter Society
Subject Category
Acoustics
Accession Number
93A29420
Funding Number(s)
PROJECT: RTOP 505-63-51
Distribution Limits
Public
Copyright
Other

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