| タイトル | Elastic buckling analysis for composite stiffened panels and other structures subjected to biaxial inplane loads |
| 本文（外部サイト） | http://hdl.handle.net/2060/19730022131 |
| 著者（英） | Tamekuni, M.; Viswanathan, A. V. |
| 著者所属（英） | Boeing Commercial Airplane Co. |
| 発行日 | 1973-09-01 |
| 言語 | eng |
| 内容記述 | An exact linear analysis method is presented for predicting buckling of structures with arbitrary uniform cross section. The structure is idealized as an assemblage of laminated plate-strip elements, curved and planar, and beam elements. Element edges normal to the longitudinal axes are assumed to be simply supported. Arbitrary boundary conditions may be specified on any external longitudinal edge of plate-strip elements. The structure or selected elements may be loaded in any desired combination of inplane transverse compression or tension side load and axial compression load. The analysis simultaneously considers all possible modes of instability and is applicable for the buckling of laminated composite structures. Numerical results correlate well with the results of previous analysis methods. |
| NASA分類 | STRUCTURAL MECHANICS |
| レポートNO | 73N30863
NASA-CR-2216 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/197879 |
