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Flutter of buckled, simply supported, rectangular panels at supersonic speedsFlutter analysis on buckled supported rectangular panels under supersonic surface flow
Document ID
19680008182
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Fralich, R. W. (NASA Langley Research Center Hampton, VA, United States)
Mc Elman, J. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1968
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-4357
Report Number: NASA-TN-D-4357
Accession Number
68N17651
Funding Number(s)
CONTRACT_GRANT: 126-14-02-24-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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