| タイトル | Minimum-weight designs for hat-stiffened composite panels under uniaxial compression |
| 本文（外部サイト） | http://hdl.handle.net/2060/19750002425 |
| 著者（英） | Agarwal, B.; Davis, R. C. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1974-11-01 |
| 言語 | eng |
| 内容記述 | Optimum hat-stiffened compression panel designs are determined by a structural synthesis technique. The effects of simplifying assumptions made in the buckling analysis for the optimization program are investigated by a linked plate element program. Optimization results for hat-stiffened graphite-epoxy panels show a 50-percent weight savings over optimized aluminum panels. Composite panels are shown to possess a variety of proportions at nearly constant weight. |
| NASA分類 | STRUCTURAL MECHANICS |
| レポートNO | 75N10497
L-9739
NASA-TN-D-7779 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/192337 |
