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Supersonic flutter of sandwich panels - Effects of face sheet bending stiffness, rotary inertia, and orthotropic core shear stiffnessesNumerical analysis of supersonic flutter of flat rectangular, biaxilly stressed sandwich panels
Document ID
19710022897
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Erickson, L. L. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1971
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-6427
A-3868
Report Number: NASA-TN-D-6427
Report Number: A-3868
Accession Number
71N32373
Funding Number(s)
CONTRACT_GRANT: 126-14-14-03-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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