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Supersonic flutter of flat rectangular orthtropic panels elastically restrained against edge rotationSupersonic flutter analysis for flat loaded orthotropic panels with edge restraint
Document ID
19660023324
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Erickson, L. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1966
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-3500
Report Number: NASA-TN-D-3500
Accession Number
66N32614
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLUTTER ANALYSIS
SUPERSONIC FLUTTER
DYNAMIC LOAD
RECTANGULAR PANEL

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