直交異方性積層材の剛性特性と最適化(円筒殻への応用)
スポンサーリンク
概要
- 論文の詳細を見る
This paper first treats the relation between in-plane and out-of-plane lamination parameters and the relation between lamination parameters and laminate configurations. Next, on the basis of these relations, the laminate configuration which gives the highest buckling stress of orthotropic laminated cylindrical shells under axial compression or external pressure is examined. It is shown that a special cross-ply laminate is the optimal laminate configuration for the buckling of cylindrical shells under external pressure.