| タイトル | Integrated technology wing design study |
| 本文（外部サイト） | http://hdl.handle.net/2060/19840025331 |
| 著者（英） | Hays, A. P.; Penrose, B. J.; Beck, W. E.; Morita, W. H.; Wainfan, B. S.; Skarshaug, R. E. |
| 著者所属（英） | Lockheed-California Co. |
| 発行日 | 1984-08-01 |
| 言語 | eng |
| 内容記述 | The technology development costs and associated benefits in applying advanced technology associated with the design of a new wing for a new or derivative trijet with a capacity for 350 passengers and maximum range of 8519 km, entering service in 1990 were studied. The areas of technology are: (1) airfoil technology; (2) planform parameters; (3) high lift; (4) pitch active control system; (5) all electric systems; (6) E to 3rd power propulsion; (7) airframe/propulsion integration; (8) graphite/epoxy composites; (9) advanced aluminum alloys; (10) titanium alloys; and (11) silicon carbide/aluminum composites. These technologies were applied to the reference aircraft configuration. Payoffs were determined for block fuel reductions and net value of technology. These technologies are ranked for the ratio of net value of technology (NVT) to technology development costs. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 84N33402
NAS 1.26:3586
NASA-CR-3586
LR-30000 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/158370 |
