Hither-to-fore an unavailable analytical solution (strong form or differential form) to the boundary-value problem of advanced fiber reinforced anti-symmetric angle-ply laminated cylindrical panels of rectangular planform subjected to static loadings is presented. A variationally consistent higher s
Free vibration of symmetric angle-ply thick laminated composite cylindrical shells
โ Scribed by K.Y. Lam; Wu Qian
- Publisher
- Elsevier Science
- Year
- 2000
- Tongue
- English
- Weight
- 178 KB
- Volume
- 31
- Category
- Article
- ISSN
- 1359-8368
No coin nor oath required. For personal study only.
โฆ Synopsis
Analytical solutions for the vibrations of thick symmetric angle-ply laminated composite cylindrical shells are established using the firstorder shear deformation theory. The complex method is developed to deal with the partial differential governing equations of thick symmetric angle-ply laminated composite cylindrical shells. Numerical results are provided for comparison, and coincide with existing results in the literature. The frequency characteristics for thick symmetric angle-ply laminated composite cylindrical shells with different H=R and L=R ratios are studied in comparison with those of symmetric cross-ply laminates. Also, the influence of lamination angle and number of lamination layers on frequency is investigated in details.
๐ SIMILAR VOLUMES
This paper reports an extension of previous work [1] to the study of the free flexural vibration analysis of symmetrically laminated triangular plates. The analysis is performed by using a simple and straightforward \(p b-2\) Rayleigh-Ritz method. A governing frequency equation for the laminated tri
Free vibrations of thick rotating cross-ply laminated composite cylindrical shells are studied based on the "rst order shear deformation shell theory (FSDT). The governing equations of "ve degrees of freedom with consideration of Coriolis accelerations and rotary inertias are established. Analytical