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General Instability of Stiffened Cylinders
| Content Provider | University of North Texas |
|---|---|
| Author | Becker, Herbert |
| Organization | United States. National Advisory Committee for Aeronautics. |
| Description | "Theoretical buckling stresses are determined in explicit form for circular cylinders with circumferential and axial stiffening. The loadings are axial compression, radial pressure, hydrostatic pressure, and torsion. Analyses were confined to moderate-length and long cylinders" (p. 1). |
| File Format | |
| Archival Resource Key | ark:/67531/metadc57302 |
| Language | English |
| Publisher Date | 2018-10-09 |
| Access Restriction | Open |
| Subject Keyword | stiffened cylinders general instability |
| Content Type | Text |
| Resource Type | Report |