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Flutter analysis of flat rectangular panels based on three-dimensional supersonic unsteady potential flowFlutter analysis of flat rectangular panels based on three-dimensional supersonic unsteady potential flow
Document ID
19670007346
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Report (TR)
Authors
Cunningham, H. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1967
Subject Category
Aerodynamics
Report/Patent Number
NASA-TR-R-256
Report Number: NASA-TR-R-256
Accession Number
67N16675
Funding Number(s)
CONTRACT_GRANT: 126-14-02-01-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
UNSTEADY FLOW
SUPERSONIC FLUTTER
PANEL FLUTTER
THREE-DIMENSIONAL FLOW
POTENTIAL FLOW

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