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EXPERIMENTAL PANEL FLUTTER RESULTS FOR SOME FLAT AND CURVED TITANIUM SKIN PANELS AT SUPERSONIC SPEEDSPanel flutter results for flat and curved titanium skin panels at supersonic speed
Document ID
19630002128
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Mc Kinney, R. L. (NASA Langley Research Center Hampton, VA, United States)
Presnell, J. G., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1963
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TN-D-1600
Report Number: NASA-TN-D-1600
Accession Number
63N12004
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PANEL FLUTTER
SUPERSONIC FLUTTER
TITANIUM
FLAT PLATE
CURVED SURFACE

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