The free vibration and dynamic response of clamped laminated curved panels subjected to the step, triangular and explosive loadings are investigated. The case of rectangular panels having fixed boundary conditions is also considered. The Rayleigh-Ritz method is employed to obtain the natural frequencies of the clamped laminated curved panels by using a set of simple polynomials as admissible functions. The normal mode superposition method is then used in the analysis of the dynamic response. Numerical results of the symmetric angle-ply, symmetric and antisymmetric cross-ply laminated curved panels under three kinds of dynamic loadings are presented.
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Hohai Univ, Dept Engn Mech, Nanjing 211100, Peoples R ChinaHohai Univ, Dept Engn Mech, Nanjing 211100, Peoples R China
Hu, Huifeng
Yu, Tiantang
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Hohai Univ, Dept Engn Mech, Nanjing 211100, Peoples R China
Jiangsu Prov Wind Power Struct Engn Res Ctr, Nanjing 211100, Peoples R ChinaHohai Univ, Dept Engn Mech, Nanjing 211100, Peoples R China
Yu, Tiantang
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Lich, Le Van
Bui, Tinh Quoc
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Duy Tan Univ, Inst Res & Dev, Da Nang City, Vietnam
Tokyo Inst Technol, Dept Civil & Environm Engn, Meguro Ku, 2-12-1-W8-22 Ookayama, Tokyo 1528552, JapanHohai Univ, Dept Engn Mech, Nanjing 211100, Peoples R China