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 |
| ISSN | 1063-7095 1573-8582 |
| DOI | 10.1007/s10778-006-0163-3 |
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| Abstract | 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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| AbstractList | 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 |
| Author | Trach, V. M. |
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| CitedBy_id | crossref_primary_10_1007_s10778_010_0283_7 crossref_primary_10_1007_s10778_008_0015_4 crossref_primary_10_1007_s10778_010_0251_2 crossref_primary_10_1088_1757_899X_471_3_032052 crossref_primary_10_1007_s10778_010_0292_6 crossref_primary_10_1007_s10778_007_0027_5 crossref_primary_10_1007_s10778_007_0065_z crossref_primary_10_1007_s10778_019_00951_5 crossref_primary_10_1007_s10778_008_0049_7 |
| Cites_doi | 10.1007/s10778-005-0136-y 10.1023/A:1015340110391 10.1023/B:INAM.0000041398.28447.45 10.1007/s10778-006-0023-1 10.1007/BF02682182 10.1023/B:INAM.0000037305.78333.21 |
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| References | R. B. Rikards (163_CR9) 1974 163_CR7 G. A. Vanin (163_CR2) 1987 E. I. Bespalova (163_CR10) 2002; 38 N. P. Semenyuk (163_CR12) 2004; 40 S. A. Ambartsumyan (163_CR1) 1974 Ya. M. Grigorenko (163_CR3) 1981 N. P. Semenyuk (163_CR11) 2005; 41 A. O. Rasskazov (163_CR8) 1999; 40 Ya. M. Grigorenko (163_CR4) 1988 A. N. Guz (163_CR6) 2001 N. P. Semenyuk (163_CR13) 2005; 41 V. D. Kubenko (163_CR5) 1999 V. M. Trach (163_CR14) 2004; 40 |
| References_xml | – volume-title: Stability of Composite Shells with Imperfections year: 1987 ident: 163_CR2 – volume: 41 start-page: 682 issue: 6 year: 2005 ident: 163_CR13 publication-title: Int. Appl. Mech. doi: 10.1007/s10778-005-0136-y – volume-title: Stability of Structural Members year: 2001 ident: 163_CR6 – volume-title: Theory of Variable-Stiffness Shells year: 1981 ident: 163_CR3 – volume-title: Dynamics of Structural Members year: 1999 ident: 163_CR5 – volume: 38 start-page: 90 issue: 1 year: 2002 ident: 163_CR10 publication-title: Int. Appl. Mech. doi: 10.1023/A:1015340110391 – volume-title: Numerical Solutions to Static Problems for Flexible Laminated Shells with Variable Parameters year: 1988 ident: 163_CR4 – volume-title: Stability of Composite Shells year: 1974 ident: 163_CR9 – volume: 40 start-page: 694 issue: 6 year: 2004 ident: 163_CR12 publication-title: Int. Appl. Mech. doi: 10.1023/B:INAM.0000041398.28447.45 – volume: 41 start-page: 1170 issue: 10 year: 2005 ident: 163_CR11 publication-title: Int. Appl. Mech. doi: 10.1007/s10778-006-0023-1 – volume-title: General Theory of Anisotropic Shells year: 1974 ident: 163_CR1 – volume: 40 start-page: 589 issue: 6 year: 1999 ident: 163_CR8 publication-title: Int. Appl. Mech. doi: 10.1007/BF02682182 – volume: 40 start-page: 573 issue: 5 year: 2004 ident: 163_CR14 publication-title: Int. Appl. Mech. doi: 10.1023/B:INAM.0000037305.78333.21 – ident: 163_CR7 |
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| Title | Stability of cylindrical shells with one plane of elastic symmetry under axial compression and torsion |
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