Buckling of composite cylindrical shells fabricated using thin-ply under axial compression
Carbon-fiber reinforced polymer (CFRP) composites possess high specific stiffness and strength and have been widely used as structural materials in aerospace and aircraft engineering. In many practical applications, such as wing skin, loading condition is a complexity of tension, bending, and torsio...
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| Main Authors: | HUANG Chun-fang, XIAO Jia-yu, HUANG Zhan-hong, ZHANG Jian-wei, JU Su, JIANG Da-zhi |
|---|---|
| Format: | Article |
| Language: | zho |
| Published: |
Science Press
2018-07-01
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| Series: | 工程科学学报 |
| Subjects: | |
| Online Access: | http://cje.ustb.edu.cn/article/doi/10.13374/j.issn2095-9389.2018.07.012 |
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