| タイトル | Composite components under impact load and effects of defects on the loading capacity |
| 本文（外部サイト） | http://hdl.handle.net/2060/19800007844 |
| 著者（英） | Wurzel, D.; Aoki, R. |
| 著者所属（英） | NASA Headquarters |
| 発行日 | 1979-09-01 |
| 言語 | eng |
| 内容記述 | Investigations were carried out on a horizontal tail assembly made of carbon fiber reinforced plastic for the Alpha Jet. The possibility of obtaining a leading edge nose design lighter but not more expensive than a metal version was studied. An important consideration was sufficient resistance of the leading edge against impact of stones and hailstones combined with high degree of stiffness. The improvement of energy reception characteristics of the materials through suitable laminate design was considered. Since certain defects occur in structural components, the effects of such defects on the characteristics of the parts were also studied. |
| NASA分類 | COMPOSITE MATERIALS |
| レポートNO | 80N16104
NASA-TM-75351
DGLR-78-190 |
| 権利 | No Copyright |
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