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Flutter at Mach 3 of thermally stressed panels and comparison with theory for panels with edge rotational restraintFlutter at Mach 3 of thermally stressed flat isotropic panels
Document ID
19660023258
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Dixon, S. C. (NASA Langley Research Center Hampton, VA, United States)
Shideler, J. L. (NASA Langley Research Center Hampton, VA, United States)
Shore, C. P. (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-3498
Report Number: NASA-TN-D-3498
Accession Number
66N32548
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC SPEED
SUPERSONIC FLOW
PANEL FLUTTER
THERMAL STRESS

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