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Flutter investigation of streamwise-oriented arrays of curved panels under compressive loading and aerodynamic heatingFlutter characteristics tested on cylindrical segments of longitudinal arrays of rectangular curved panels under compressive loading and aerodynamic heating
Document ID
19650018216
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Deveikis, W. D. (NASA Langley Research Center Hampton, VA, United States)
Rosecrans, R. (NASA Langley Research Center Hampton, VA, United States)
Walker, R. W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1965
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-2910
Report Number: NASA-TN-D-2910
Accession Number
65N27817
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
COMPRESSION LOADING
PANEL FLUTTER
AERODYNAMIC HEATING
FLUTTER ANALYSIS
RECTANGULAR PANEL

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