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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
19910016097
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Seybert, A. F.
(Kentucky Univ. Lexington., United States)
Wu, T. W.
(Kentucky Univ. Lexington., United States)
Wu, X. F.
(Kentucky Univ. Lexington., United States)
Oswald, Fred B.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1991
Subject Category
Mechanical Engineering
Report/Patent Number
AVSCOM-TR-90-C-002
NASA-TM-103691
E-5910
NAS 1.15:103691
Report Number: AVSCOM-TR-90-C-002
Report Number: NASA-TM-103691
Report Number: E-5910
Report Number: NAS 1.15:103691
Meeting Information
Meeting: American Helicopter Society Technical Specialists Meeting
Location: Philadelphia, PA
Country: United States
Start Date: October 15, 1991
End Date: October 16, 1991
Accession Number
91N25411
Funding Number(s)
PROJECT: DA PROJ. 1L1-62209-A-47A
PROJECT: RTOP 505-63-51
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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