摘要
本文运用Reddy[1]的高阶位移模式剪切变形理论,得出了具有弹性转动约束边界条件的正交对称铺设层合板的弯曲解。利用稀疏矩阵技术求解大型稀疏线性方程组。同三维弹性理论解相比,本方法所产生的误差很小。
Based on the Reddy-type plate theory of higher-order shear deformation ,a solution is formulated for symmetrically laminated cross-ply rectangular plate with edges elastically restrained against rotation.Large sparse system of linear equations are solved by sparse matrix methods.The present theory leads to less error when compared with three-dimensional elasticity solutions.
出处
《南昌航空工业学院学报》
CAS
1998年第2期1-8,共8页
Journal of Nanchang Institute of Aeronautical Technology(Natural Science Edition)
关键词
弹性转动约束
复合材料
层合板
弯曲
elasticity, rotation,constraints ,composite materials,laminated plates