Stability of cylindrical shells with one plane of elastic symmetry under axial compression and torsion
A numerical technique is developed for stability analysis of laminated cylindrical shells with one plane of symmetry subject to axial compression and torsion. Shells filament-wound in directions other than the coordinate axes are considered as a special case. These shells are analyzed for stability...
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| Published in | International applied mechanics Vol. 42; no. 8; pp. 943 - 947 |
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| Main Author | |
| Format | Journal Article |
| Language | English |
| Published |
01.08.2006
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| Online Access | Get full text |
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| Summary: | A numerical technique is developed for stability analysis of laminated cylindrical shells with one plane of symmetry subject to axial compression and torsion. Shells filament-wound in directions other than the coordinate axes are considered as a special case. These shells are analyzed for stability under axial compression, external pressure, and torsion. It is shown that shells with a great number of plies and different ply angles may be considered orthotropic |
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| Bibliography: | ObjectType-Article-2 SourceType-Scholarly Journals-1 ObjectType-Feature-1 content type line 23 |
| ISSN: | 1063-7095 1573-8582 |
| DOI: | 10.1007/s10778-006-0163-3 |