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RECENT RESEARCH IN BUCKLING OF CYLINDRICAL SHELLSResults from five separate investigations on buckling and collapse of cylindrical shells suitable for structural components of missiles and launch vehicles
Document ID
19630021004
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Peterson, J. P.
Stein, M.
Date Acquired
August 1, 2013
Publication Date
April 3, 1963
Subject Category
General
Report/Patent Number
AIAA PAPER 2903-63
Report Number: AIAA PAPER 2903-63
Accession Number
63A17063
Distribution Limits
Public
Copyright
Other
Keywords
STRUCTURAL FAILURE
LAUNCH VEHICLE
STRUCTURAL FATIGUE
BUCKLING

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