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Research investigations of bulkhead cylindri- cal junctions exposed to combined load, cryo- genic temperature. part iv- theoretical analysis of the buckling problemCompression buckling of shell of revolution under axial compression - shell stability
Document ID
19650017691
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wagner, H. (Florida Univ. Gainesville, FL, United States)
Wu, T.-T. (Florida Univ. Gainesville, FL, United States)
Date Acquired
August 2, 2013
Publication Date
August 1, 1965
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-63477
Report Number: NASA-CR-63477
Accession Number
65N27292
Funding Number(s)
CONTRACT_GRANT: NAS8-5199
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AXIAL COMPRESSION
SHELL STABILITY
COMPRESSION BUCKLING

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