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A modified VAPEPS method for predicting vibroacoustic response of unreinforced mass loaded honeycomb panelsVAPEPS (VibroAcoustic Payload Environment Prediction System) is a computer program used to predict the vibroacoustic response of a structure. An alternate VAPEPS modeling technique, the Modified NASA Lewis Method, is an improvement for modeling unreinforced mass loaded honeycomb panels. The Modified NASA Lewis Method prediction is compared to the standard ASMS VAPEPS prediction, and the acoustic test data for three spacecraft panels. An analytical method of computing variance is presented and used to compute 95 percent confidence levels. These levels are compared to the standard VAPEPS confidence levels and to the envelope of the test data. As a result of using the new methodology suggested in the paper, both the mean prediction and the 95 percent confidence level prediction agree well with the test data in both spectral shape and magnitude. Therefore, the Modified NASA Lewis Method prediction methodology may be used to define more realistic random vibration test levels.
Document ID
19890007534
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mcnelis, Mark E.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1989
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:101467
E-4579
NASA-TM-101467
Report Number: NAS 1.15:101467
Report Number: E-4579
Report Number: NASA-TM-101467
Meeting Information
Meeting: Technical Meeting of the Inst. of Environmental Sciences
Location: Anaheim, CA
Country: United States
Start Date: May 1, 1989
End Date: May 5, 1989
Accession Number
89N16905
Funding Number(s)
PROJECT: RTOP 474-12-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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