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NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...

NASA-TM-108399 Preliminary Analysis Techniques for Ring and Stringer Stiffened Cylindrical Shells

NASA-TM-108399 Preliminary Analysis Techniques for Ring and Stringer Stiffened Cylindrical Shells
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  • 112 Downloads
  • 3.00 MB File Size
  • 1 File Count
  • 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

NASA-TM-108399 Preliminary Analysis Techniques for Ring and Stringer Stiffened Cylindrical Shells
  • Version
  • 112 Downloads
  • 3.00 MB File Size
  • 1 File Count
  • May 19, 2020 Create Date
  • May 19, 2020 Last Updated
Scroll for Details

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.

FileAction
NASA-TM-108399 Preliminary Analysis Techniques for Ring and Stringer Stiffened Cylindrical Shells.pdfDownload 
17,005 Documents in our Technical Library
2475529 Total Downloads

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Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...