Vibration analysis of thin-walled composite beams with I-shaped cross-sections
β Scribed by Thuc Phuong Vo; Jaehong Lee; Kihak Lee; Namshik Ahn
- Publisher
- Elsevier Science
- Year
- 2011
- Tongue
- English
- Weight
- 875 KB
- Volume
- 93
- Category
- Article
- ISSN
- 0263-8223
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β¦ Synopsis
A general analytical model applicable to the vibration analysis of thin-walled composite I-beams with arbitrary lay-ups is developed. Based on the classical lamination theory, this model has been applied to the investigation of load-frequency interaction curves of thin-walled composite beams under various loads. The governing differential equations are derived from the Hamilton's principle. A finite element model with seven degrees of freedoms per node is developed to solve the problem. Numerical results are obtained for thin-walled composite I-beams under uniformly distributed load, combined axial force and bending loads. The effects of fiber orientation, location of applied load, and types of loads on the natural frequencies and load-frequency interaction curves as well as vibration mode shapes are parametrically studied.
π SIMILAR VOLUMES
Lateral buckling of thin-walled composite beams with monosymmetric sections is studied. A general geometrically nonlinear model for thinwalled laminated composites with arbitrary open cross-section and general laminate stacking sequences is given by using systematic variational formulation based on