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Theoretical considerations of some nonlinear aspects of hypersonic panel flutter Annual report, 1 Sep. 1967 - 31 Aug. 1968Stability and postcritical response of infinite width panels on hinged supports due to aerodynamic loads at hypersonic speed
Document ID
19710005866
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lerner, J. I. (Stanford Univ. CA, United States)
Mc Intosh, S. C., Jr. (Stanford Univ. CA, United States)
Date Acquired
August 6, 2013
Publication Date
August 31, 1968
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-115854
AR-3
Report Number: NASA-CR-115854
Report Number: AR-3
Accession Number
71N15341
Funding Number(s)
CONTRACT_GRANT: NGR-05-020-102
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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