| タイトル | Use of statical indentation laws in the impact analysis of laminated composite plates |
| 著者（英） | Sun, C. T.; Tan, T. M. |
| 著者所属（英） | Purdue Univ.|Drexel Univ. |
| 発行日 | 1985-03-01 |
| 言語 | eng |
| 内容記述 | The low-velocity impact response of graphite/epoxy laminates was investigated theoretically and experimentally. A nine-node isoparametric plate finite element in conjunction with an empirical contact law was used for the theoretical investigation. Theoretical results are in good agreement with strain-gage experimental data. The results of the investigation indicate that the present theoretical procedure describes the impact response of laminate for low-impact velocities. |
| NASA分類 | COMPOSITE MATERIALS |
| レポートNO | 85A29133 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/392238 |
|
