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Preliminary Analysis Techniques for Ring and Stringer Stiffened Cylindrical ShellsThis report outlines methods of analysis for the buckling of thin-walled circumferentially and longitudinally stiffened cylindrical shells. Methods of analysis for the various failure modes are presented in one cohesive package. Where applicable, more than one method of analysis for a failure mode is presented along with standard practices. The results of this report are primarily intended for use in launch vehicle design in the elastic range. A Microsoft Excel worksheet with accompanying macros has been developed to automate the analysis procedures.
Document ID
19930013915
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
J Graham
(Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1993
Subject Category
Structural Mechanics
Report/Patent Number
Report Number: NASA-TM-108399
Report Number: NAS 1.15:108399
NASA-TM-108399
NAS 1.15:108399
Accession Number
93N23104
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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