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Flutter design of stiffened-skin panels for hypersonic aircraftDesign factors for flutter control of stiffened exterior skin panels for hypersonic aircraft
Document ID
19700003020
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Anderson, M. S. (NASA Langley Research Center Hampton, VA, United States)
Bohon, H. L. (NASA Langley Research Center Hampton, VA, United States)
Heard, W. L., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1969
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-5555
Report Number: NASA-TN-D-5555
Accession Number
70N12324
Funding Number(s)
CONTRACT_GRANT: 126-14-14-06-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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