| タイトル | Some applications of NASTRAN to the buckling of thin cylindrical shells with cutouts |
| 本文（外部サイト） | http://hdl.handle.net/2060/19720025224 |
| 著者（英） | Starnes, J. H., Jr.; Williams, J. G. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1972-09-01 |
| 言語 | eng |
| 内容記述 | The buckling of isotropic and waffle-stiffened circular cylinders with and without cutouts was studied using NASTRAN's Rigid Format 5 for the case of axial compressive loading. The results obtained for the cylinders without cutouts are compared with available reference solutions. The results for the isotropic cylinders containing a single circular cutout with selected radii are compared with available experimental data. For the waffle-stiffened cyclinder, the effect of two diametrically opposed rectangular cutouts was studied. A DMAP alter sequence was used to permit the necessary application of different prebuckling and buckling boundary conditions. Advantage was taken of available symmetry planes to formulate equivalent NASTRAN model segments which reduced the associated computational cost of performing the analyses. Limitations of the applicability of NASTRAN for the solution of problems with nonlinear characteristics are discussed. |
| NASA分類 | STRUCTURAL MECHANICS |
| レポートNO | 72N32874 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/570682 |
