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The general instability of ring-stiffened corrugated cylinders under axial compressionDetermining general instability load of ring stiffened corrugated cylinder under axial compression by linear small deflection theory
Document ID
19660005097
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Brolliar, R. H. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Dickson, J. N. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1966
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-3089
Report Number: NASA-TN-D-3089
Accession Number
66N14386
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CYLINDRICAL SHELL
COMPRESSION BUCKLING
CORRUGATED SHELL
SHELL STABILITY
AXIAL COMPRESSION

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