| タイトル | Composite structural materials |
| 本文（外部サイト） | http://hdl.handle.net/2060/19830009326 |
| 著者（英） | Loewy, R. G.; Wiberley, S. E.; Ansell, G. S. |
| 著者所属（英） | Rensselaer Polytechnic Inst. |
| 発行日 | 1982-12-01 |
| 言語 | eng |
| 内容記述 | The promise of filamentary composite materials, whose development may be considered as entering its second generation, continues to generate intense interest and applications activity. Fiber reinforced composite materials offer substantially improved performance and potentially lower costs for aerospace hardware. Much progress has been achieved since the initial developments in the mid 1960's. Rather limited applications to primary aircraft structure have been made, however, mainly in a material-substitution mode on military aircraft, except for a few experiments currently underway on large passenger airplanes in commercial operation. To fulfill the promise of composite materials completely requires a strong technology base. NASA and AFOSR recognize the present state of the art to be such that to fully exploit composites in sophisticated aerospace structures, the technology base must be improved. This, in turn, calls for expanding fundamental knowledge and the means by which it can be successfully applied in design and manufacture. |
| NASA分類 | COMPOSITE MATERIALS |
| レポートNO | 83N17597
NAS 1.26:169859
NASA-CR-169859
SAR-43 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/163565 |
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