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Flexural response of doubly curved laminated composite shells

Flexural response of doubly curved laminated composite shells
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摘要 In the present work, analytical solutions for laminated composite doubly curved panels on rectangular plan form undergoing small deformations and subjected to uniformly distributed transverse load have been obtained. The problem is formulated using first order shear deformation theory. The spatial descretization of the linear differential equations is carried out using fast converging finite double Chebyshev series. The effect of panel thickness, curvature, boundary conditions, lamination scheme as well as material property on the static response of panel has been investigated in detail. In the present work, analytical solutions for laminated composite doubly curved panels on rectangular plan form undergoing small deformations and subjected to uniformly distributed transverse load have been obtained. The problem is formulated using first order shear deformation theory. The spatial descretization of the linear differential equations is carried out using fast converging finite double Chebyshev series. The effect of panel thickness, curvature, boundary conditions, lamination scheme as well as material property on the static response of panel has been investigated in detail.
出处 《Science China(Physics,Mechanics & Astronomy)》 SCIE EI CAS 2013年第4期812-817,共6页 中国科学:物理学、力学、天文学(英文版)
关键词 doubly curved panel analytical CHEBYSHEV STATIC rectangular plan form 复合材料 弯曲响应 层合壳 双曲面 一阶剪切变形理论 线性微分方程 均匀分布 横向载荷
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参考文献13

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