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Flutter of curved and flat sandwich panels subjected to supersonic flowFlutter characteristics of curved and flat sandwich panels subjected to supersonic flow
Document ID
19640009808
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Mc Elman, J. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1964
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TN-D-2192
Report Number: NASA-TN-D-2192
Accession Number
64N19722
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SANDWICH CONSTRUCTION
SUPERSONIC FLOW
PANEL FLUTTER

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