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ON EDGE BUCKLING OF AXIALLY-COMPRESSED, CIRCULAR CYLINDRICAL SHELLS.On edge buckling of axially compressed, circular cylindrical shells
Document ID
19620000969
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hoff, N. J. (Stanford Univ. CA, United States)
Nachbar, W. (Stanford Univ. CA, United States)
Date Acquired
August 1, 2013
Publication Date
November 1, 1961
Subject Category
Structural Mechanics
Report/Patent Number
SUDAER-115
Report Number: SUDAER-115
Accession Number
62N10969
Funding Number(s)
CONTRACT_GRANT: NSG-93-60
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
EDGE
AXIAL COMPRESSION
CYLINDRICAL SHELL
SHELL
CIRCULAR SHELL
COMPRESSION
BUCKLING
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