A semi analytical method for free vibration analysis of composite laminated cylindrical and spherical shells with complex boundary conditions. (March 2019)

• Record Type: Journal Article
• Authors: Li, Haichao; Pang, Fuzhen; Miao, Xuhong; Gao, Shengyao; Liu, Feng
• Is Part Of: Thin-walled structures. Volume 136(2019)
• Page Start: 200
• Page End: 220
• Publication Date: 2019-03
• Subjects: Free vibration -- Composite laminated cylindrical and spherical shells -- Penalty method -- Jacobi polynomials -- Complex boundary conditions; Thin-walled structures -- Periodicals; 690.1
• DOI: 10.1016/j.tws.2018.12.009
• Languages: English
• ISSNs: 0263-8231

Abstract

Abstract: A semi analytical method is employed to analyze free vibration behaviors of composite laminated cylindrical and spherical shells subject to complex boundary conditions. The analytical model is established on the basis of multi-segment partitioning strategy and first-order shear deformation theory. The displacement functions are made up of the Jacobi polynomials along axial direction and Fourier series along circumferential direction. In order to obtain continuity conditions and satisfy complex boundary conditions, the penalty method about spring technique is adopted. The solutions about free vibration behaviors of composite laminated cylindrical and spherical shells were obtained by approach of Rayleigh–Ritz. The convergence study and numerical verifications for composite laminated cylindrical and spherical shells with different boundary conditions, Jacobi parameters, spring parameters and truncation of permissible displacement functions are carried out. Through the comparison and analysis study, it is obvious that the proposed method has a good stable and rapid convergence property and the results of this paper closely agreed with those obtained by published literatures, FEM and experiment. In addition, some interesting results about free vibration characteristics of composite laminated cylindrical and spherical shells are investigated. Highlights: Free vibration of composite laminated cylindrical and spherical shells is investigated by using a semi-analytical method. The paper presents a generalized formulation for free vibration analysis of composite laminated shells. The paper generalizes the selection of the admissible displacement functions by using the Jacobi polynomial.