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Supersonic flutter of simply supported isotropic sandwich panelsTwo-dimensional static aerodynamics for determining supersonic flutter characteristics of simply supported isotropic sandwich panels
Document ID
19660012982
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Anderson, M. S. (NASA Langley Research Center Hampton, VA, United States)
Erickson, L. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1966
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-3171
Accession Number
66N22271
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC FLUTTER
STATIC AERODYNAMIC CHARACTERISTICS
RECTANGULAR PANEL
NUMERICAL ANALYSIS
SANDWICH CONSTRUCTION

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