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Comparison of panel flutter results from approximate aerodynamic theory with results from exact inviscid theory and experimentComparison of panel flutter results from approximate aerodynamic theory with results from exact inviscid theory and experiment
Document ID
19660029122
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Dixon, S. C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1966
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-3649
Accession Number
66N38412
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PANEL FLUTTER
AERODYNAMICS
FLUTTER ANALYSIS

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