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Response of space shuttle insulation panels to acoustic noise pressureThe response of reusable space shuttle insulation panels to random acoustic pressure fields are studied. The basic analytical approach in formulating the governing equations of motion uses a Rayleigh-Ritz technique. The input pressure field is modeled as a stationary Gaussian random process for which the cross-spectral density function is known empirically from experimental measurements. The response calculations are performed in both frequency and time domain.
Document ID
19760018239
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Vaicaitis, R.
(Columbia Univ. New York, NY, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1976
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-148201
FR-2
Accession Number
76N25327
Funding Number(s)
CONTRACT_GRANT: NSG-1059
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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