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Supersonic flutter of a thermally stressed flat panel with uniform edge loadsSupersonic flutter of thermally stressed flat panel with uniform edge loads
Document ID
19650026357
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Heard, W. L., Jr. (NASA Langley Research Center Hampton, VA, United States)
Schaeffer, H. G. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1965
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-3077
Report Number: NASA-TN-D-3077
Accession Number
65N35958
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC FLUTTER
EDGE LOADING
FLUTTER ANALYSIS
PANEL FLUTTER

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