Buckling design of stiffened cylindrical shells under axial compression based on energy barrier approach
Buckling design of axially compressed cylindrical shells is still a challenging subject due to the well-known imperfection sensitivity characteristic. Compared to the unstiffened ones, design of buckling loads for the stiffened cylindrical shells composed of skins and stiffeners is more difficult co...
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| Published in | Thin-walled structures Vol. 179; p. 109667 |
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| Main Authors | , , , , |
| Format | Journal Article |
| Language | English |
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Elsevier Ltd
01.10.2022
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| Abstract | Buckling design of axially compressed cylindrical shells is still a challenging subject due to the well-known imperfection sensitivity characteristic. Compared to the unstiffened ones, design of buckling loads for the stiffened cylindrical shells composed of skins and stiffeners is more difficult considering about the complicated effects of structural parameters on the imperfection sensitivity. In this paper, the promising buckling design method based on energy barrier approach is applied to the axially compressed stiffened cylindrical shells. Three manufactured stiffened cylindrical shells from references are selected to verify the reliability of the method by comparing with the existing experimental data. In addition, various stiffened cylindrical shell models with dimple imperfections are designed and numerically researched in this paper to further prove the reliable design buckling loads provided by this method. The buckling loads designed by other similar methods are also taken for comparison. Results have verified the reliability and advantage of the method in this paper for clarifying imperfection sensitivity and designing buckling loads of stiffened cylindrical shells. Then, using this method, the complicated effects of different structural parameters on the imperfection sensitivity and design buckling loads of the stiffened cylindrical shells are systematically investigated. Based on that, the stiffened cylindrical shells with both high design buckling loads and quite low imperfection sensitivity which are always favorable in lightweight design have been successfully obtained. It also indicates a potential improvement for the load-carrying efficiency of current stiffened cylindrical shells using the buckling design method based on energy barrier approach.
•Buckling design of stiffened cylindrical shells by energy barrier approach is presented.•Reliability and advantage of the buckling design method are verified by numerical and existing experimental results.•Parametric effects on design buckling loads of stiffened cylindrical shells are clarified.•The cylindrical shells with both high buckling loads and low imperfection sensitivity are obtained. |
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| AbstractList | Buckling design of axially compressed cylindrical shells is still a challenging subject due to the well-known imperfection sensitivity characteristic. Compared to the unstiffened ones, design of buckling loads for the stiffened cylindrical shells composed of skins and stiffeners is more difficult considering about the complicated effects of structural parameters on the imperfection sensitivity. In this paper, the promising buckling design method based on energy barrier approach is applied to the axially compressed stiffened cylindrical shells. Three manufactured stiffened cylindrical shells from references are selected to verify the reliability of the method by comparing with the existing experimental data. In addition, various stiffened cylindrical shell models with dimple imperfections are designed and numerically researched in this paper to further prove the reliable design buckling loads provided by this method. The buckling loads designed by other similar methods are also taken for comparison. Results have verified the reliability and advantage of the method in this paper for clarifying imperfection sensitivity and designing buckling loads of stiffened cylindrical shells. Then, using this method, the complicated effects of different structural parameters on the imperfection sensitivity and design buckling loads of the stiffened cylindrical shells are systematically investigated. Based on that, the stiffened cylindrical shells with both high design buckling loads and quite low imperfection sensitivity which are always favorable in lightweight design have been successfully obtained. It also indicates a potential improvement for the load-carrying efficiency of current stiffened cylindrical shells using the buckling design method based on energy barrier approach.
•Buckling design of stiffened cylindrical shells by energy barrier approach is presented.•Reliability and advantage of the buckling design method are verified by numerical and existing experimental results.•Parametric effects on design buckling loads of stiffened cylindrical shells are clarified.•The cylindrical shells with both high buckling loads and low imperfection sensitivity are obtained. |
| ArticleNumber | 109667 |
| Author | Li, Longhua Hu, Dapeng Gu, Wenguang Liu, Peiqi Fan, Haigui |
| Author_xml | – sequence: 1 givenname: Haigui surname: Fan fullname: Fan, Haigui email: haigui@dlut.edu.cn – sequence: 2 givenname: Longhua surname: Li fullname: Li, Longhua – sequence: 3 givenname: Wenguang surname: Gu fullname: Gu, Wenguang – sequence: 4 givenname: Peiqi surname: Liu fullname: Liu, Peiqi – sequence: 5 givenname: Dapeng surname: Hu fullname: Hu, Dapeng |
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| Keywords | Knockdown factor Imperfection sensitivity Axial compression Buckling Stiffened cylindrical shell |
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| SubjectTerms | Axial compression Buckling Imperfection sensitivity Knockdown factor Stiffened cylindrical shell |
| Title | Buckling design of stiffened cylindrical shells under axial compression based on energy barrier approach |
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