FURTHER CREEP BUCKLING TESTS WITH CYLINDERS SUBJECTED TO FLEXURE,
Abstract
Twenty-nine circular cylindrical shells manufactured of 5052-0 aluminum alloy were tested in pure bending at a temperature of 500F. Ten of these were unreinforced, nine had longitudinal, and ten longitudinal and circumferential reinforcing elements. All the specimens failed in creep buckling. The results of the experiments are presented in tables and diagrams. A few theoretical considerations are given in three appendices. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 01, 1957
- Accession Number
- AD0686439
Entities
People
- Burton Erickson
- Francis W. French
Organizations
- New York University Tandon School of Engineering