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Experimental and theoretical results for buckling of eccentrically stiffened cylindersBuckling strength of eccentrically stiffened cylindrical shells under axial compression
Document ID
19660027866
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Card, M. F. (NASA Langley Research Center Hampton, VA, United States)
Jones, R. M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1966
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-3639
Report Number: NASA-TN-D-3639
Accession Number
66N37156
Funding Number(s)
CONTRACT_GRANT: 124-11-06-04-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ECCENTRICITY
COMPRESSION BUCKLING
CYLINDRICAL SHELL
STIFF STRUCTURE

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