Vo, Thuc and Lee, Jaehong (2013) Vibration and buckling of thin-walled composite I-beams with arbitrary lay-ups under axial loads and end moments. Mechanics of Advanced Materials and Structures, 20 (8). pp. 652-665. ISSN 1537-6494
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Abstract
A finite element model with seven degrees of freedom per node is developed to study vibration and buckling of thin-walled composite I-beams with arbitrary lay-ups under constant axial loads and equal end moments. This model is based on the classical lamination theory, and accounts for all the structural coupling coming from material anisotropy. The governing differential equations are derived from the Hamilton’s principle. Numerical results are obtained for thin-walled composite I-beams to investigate the effects of axial force, bending moment and fiber orientation on the buckling moments, natural frequencies, and corresponding vibration mode shapes as well as axial-moment-frequency interaction curves.
| Item Type: | Article |
|---|---|
| Uncontrolled Keywords: | thin-walled composite I-beams, fiber orientation, axial loads, end moments, axial-moment-frequency interaction curves |
| Subjects: | H200 Civil Engineering H300 Mechanical Engineering H400 Aerospace Engineering |
| Department: | Faculties > Engineering and Environment > Mechanical and Construction Engineering |
| Depositing User: | Thuc Vo |
| Date Deposited: | 04 Sep 2013 10:37 |
| Last Modified: | 17 Dec 2023 14:34 |
| URI: | https://nrl.northumbria.ac.uk/id/eprint/13390 |
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