| タイトル | Influence of an asymmetric ring on the modeling of an orthogonally stiffened cylindrical shell |
| 本文（外部サイト） | http://hdl.handle.net/2060/19940029756 |
| 著者（英） | Rastogi, Naveen; Johnson, Eric R. |
| 著者所属（英） | Virginia Polytechnic Inst. and State Univ. |
| 発行日 | 1994-01-01 |
| 言語 | eng |
| 内容記述 | Structural models are examined for the influence of a ring with an asymmetrical cross section on the linear elastic response of an orthogonally stiffened cylindrical shell subjected to internal pressure. The first structural model employs classical theory for the shell and stiffeners. The second model employs transverse shear deformation theories for the shell and stringer and classical theory for the ring. Closed-end pressure vessel effects are included. Interacting line load intensities are computed in the stiffener-to-skin joints for an example problem having the dimensions of the fuselage of a large transport aircraft. Classical structural theory is found to exaggerate the asymmetric response compared to the transverse shear deformation theory. |
| NASA分類 | STRUCTURAL MECHANICS |
| レポートNO | 94N34262
NASA-CR-195953
NAS 1.26:195953 |
| 権利 | No Copyright |
