| Nonlinear Dynamic Buckling of Damaged Composite Cylindrical Shells |
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| 作者姓名： | 王天霖 唐文勇 张圣坤 |
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| 作者单位： | State Key Laboratory of Ocean Eng. Shanghai Jiaotong Univ.，State Key Laboratory of Ocean Eng.，Shanghai Jiaotong Univ.，State Key Laboratory of Ocean Eng.，Shanghai Jiaotong Univ.，Shanghai 200030 China，Shanghai 200030 China，Shanghai 200030 China |
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| 摘 要： | Based on the first order shear deformation theory(FSDT), the nonlinear dynamic equations involving transverse shear deformation and initial geometric imperfections were obtained by Hamilton's philosophy. Geometric deformation of the composite cylindrical shell was treated as the initial geometric imperfection in the dynamic equations, which were solved by the semi-analytical method in this paper. Stiffness reduction was employed for the damaged sub-layer, and the equivalent stiffness matrix was obtained for the delaminated area. By circumferential Fourier series expansions for shell displacements and loads and by using Galerkin technique, the nonlinear partial differential equations were transformed to ordinary differential equations which were finally solved by the finite difference method. The buckling was judged from shell responses by B-R criteria, and critical loads were then determined. The effect of the initial geometric deformation on the dynamic response and buckling of composite cylindrical shell was also discussed, as well as the effects of concomitant delamination and sub-layer matrix damages.
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| 关 键 词： | 复合材料 圆柱外壳 损伤 动力反应 |
| 文章编号： | 1007-1172（2007）01-0066-07 |
| 修稿时间： | 2005-11-02 |
Nonlinear Dynamic Buckling of Damaged Composite Cylindrical Shells |
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| WANG Tian-lin,TANG Wen-yong,ZHANG Sheng-kun.Nonlinear Dynamic Buckling of Damaged Composite Cylindrical Shells[J].Journal of Shanghai Jiaotong university,2007,12(1):66-72. |
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| Authors: | WANG Tian-lin TANG Wen-yong ZHANG Sheng-kun |
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| Institution: | State Key Laboratory of Ocean Eng. , Shanghai Jiaotong Univ. , Shanghai 200030, China |
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| Abstract: | Based on the first order shear deformation theory(FSDT), the nonlinear dynamic equations involving transverse shear deformation and initial geometric imperfections were obtained by Hamilton's philosophy. Geometric deformation of the composite cylindrical shell was treated as the initial geometric imperfection in the dynamic equations, which were solved by the semi-analytical method in this paper. Stiffness reduction was employed for the damaged sub-layer, and the equivalent stiffness matrix was obtained for the delaminated area. By circumferential Fourier series expansions for shell displacements and loads and by using Galerkin technique, the nonlinear partial differential equations were transformed to ordinary differential equations which were finally solved by the finite difference method. The buckling was judged from shell responses by B-R criteria, and critical loads were then determined. The effect of the initial geometric deformation on the dynamic response and buckling of composite cylindrical shell was also discussed, as well as the effects of concomitant delamination and sub-layer matrix damages. |
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| Keywords: | composite materials cylindrical shell damage dynamic response dynamic buckling semi-analytical method |
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