A finite element analysis for the free vibration behaviour of point supported laminated composite cylindrical shells is presented. Eight-noded curved quadrilateral isoparametric elements are used. The formulation is based on the assumptions of the first order shear deformation theory for thin, shall
FINITE ELEMENT FREE VIBRATION ANALYSIS OF DOUBLY CURVED LAMINATED COMPOSITE SHELLS
โ Scribed by D. Chakravorty; J.N. Bandyopadhyay; P.K. Sinha
- Publisher
- Elsevier Science
- Year
- 1996
- Tongue
- English
- Weight
- 409 KB
- Volume
- 191
- Category
- Article
- ISSN
- 0022-460X
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โฆ Synopsis
A finite element analysis for the free vibration behaviour of doubly curved shells is presented in which eight-noded curved quadrilateral isoparametric finite elements are used. The first order shear deformation theory for thin and shallow shells is used in the formulation. Results are obtained for comparison with those in the existing literature and to investigate the effects of various composite parameters relevant to doubly curved shells, such as fibre orientations and lamination schemes and several geometrical parameters like aspect ratio, smaller height to greater height ratio (for conoids), thickness to radius ratio (for hyperbolic and elliptic paraboloids), and radii of curvature ratio (for elliptic paraboloids).
๐ SIMILAR VOLUMES
This paper presents the first endeavour to apply the global method of generalized differential quadrature (CDQ) to the free vibration analysis of composite laminated conical shells. The GDQ method has been developed to improve the differential quadrature (DQ) technique for the computation of weighti
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