NASA-TM-108399 Preliminary Analysis Techniques for Ring and Stringer Stiffened Cylindrical Shells
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- May 19, 2020 Create Date
- May 19, 2020 Last Updated
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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. These programs are available by request from the author.
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| NASA-TM-108399 Preliminary Analysis Techniques for Ring and Stringer Stiffened Cylindrical Shells.pdf | Download |
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