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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
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Graham, J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1993
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:108399
NASA-TM-108399
Accession Number
93N23104
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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