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The Twisting of Thin-Walled, Stiffened Circular Cylinders
| Content Provider | University of North Texas |
|---|---|
| Author | Schapitz, E. |
| Organization | United States. National Advisory Committee for Aeronautics. |
| Description | On the basis of the present investigation of the twisting of thin-walled, stiffened cylinders the following conclusions can be reached: 1) there is as yet no generally applicable formula for the buckling moment of the skin; 2) the mathematical treatment of the condition of the shell after buckling of the skin is based on the tension-field theory, wherein the strain condition is considered homogenous. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc63291 |
| Language | English |
| Publisher Date | 2018-09-28 |
| Access Restriction | Open |
| Subject Keyword | twisting thin-walled cylinders stress testing |
| Content Type | Text |
| Resource Type | Report |
