NASA NTRS ยท 19930013915
Preliminary analysis techniques for ring and stringer stiffened cylindrical shells
Abstract
This 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.
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Graham, J.. 1993-03-01. Preliminary analysis techniques for ring and stringer stiffened cylindrical shells. https://ntrs.nasa.gov/citations/19930013915
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