| タイトル | Advanced composites in sailplane structures: Application and mechanical properties |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790018908 |
| 著者（英） | Muser, D. |
| 著者所属（英） | Deutsche Forschungs- und Versuchsanstalt fuer Luft- und Raumfahrt |
| 発行日 | 1979-06-01 |
| 言語 | eng |
| 内容記述 | Advanced Composites in sailplanes mean the use of carbon and aramid fibers in an epoxy matrix. Weight savings were in the range of 8 to 18% in comparison with glass fiber structures. The laminates will be produced by hand-layup techniques and all material tests were done with these materials. These values may be used for calculation of strength and stiffness, as well as for comparison of the materials to get a weight-optimum construction. Proposals for material-optimum construction are mentioned. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 79N27079 |
| 権利 | No Copyright |
