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FLUTTER TESTS OF SANDWICH-TYPE FLAT PANELS AT MACH NUMBERS OF 2.97 AND 4.12Flutter tests of sandwich-type flat panels at supersonic speeds
Document ID
19630002624
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Evans, E. W. (NASA Langley Research Center Hampton, VA, United States)
Kordes, E. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1958
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-MEMO-10-17-58L
Report Number: NASA-MEMO-10-17-58L
Accession Number
63N12500
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLUTTER
AEROELASTICITY
SUPERSONIC FLOW
PANEL FLUTTER
SANDWICH CONSTRUCTION
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