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Critical combinations of torsion and direct axial stress for thin-walled cylinders /
A theoretical solution is presented for the determination of the combinations of direct axial stress and torsion which cause thin-walled cylinders with either simply supported or clamped edges to buckle. This theoretical solution is used in conjunction with available test data to develop empirical c...
| Call Number: | Libro Electrónico |
|---|---|
| Main Author: | |
| Corporate Author: | |
| Other Authors: | , |
| Format: | Government Document Electronic eBook |
| Language: | Inglés |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1947.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 1345. |
| Subjects: | |
| Online Access: | Texto completo |