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Anti-symmetric angle-ply laminated thick cylindrical panels

โœ Scribed by H.R.H. Kabir


Publisher
Elsevier Science
Year
1998
Tongue
English
Weight
847 KB
Volume
35
Category
Article
ISSN
0020-7683

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โœฆ Synopsis


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 shell theory is utilized that generates five highly coupled fourth order partial differential equations in five unknowns, three displacements, and two rotations. A boundary continuous double Fourier series-based solution functions is assumed to solve such equations in conjunction with the admissible boundary conditions. The numerical results constitute the study of convergence of displacements, in-plane forces, and moments ; and spatial variations of them presented in the form of contour plotting for various parametric effects. These, hither-to unavailable solutions, and analytically obtained numerical results should serve as bench-marks for future comparisons of popular approximate methods (integral form or weak form), such as finite element, boundary element, finite difference, Galerkin approach, Rayleigh-Ritz, collocation, least-squares methods, and experimental results, etc.


๐Ÿ“œ SIMILAR VOLUMES


Free vibration of symmetric angle-ply th
โœ K.Y. Lam; Wu Qian ๐Ÿ“‚ Article ๐Ÿ“… 2000 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 178 KB

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