| タイトル | On a global aerodynamic optimization of a civil transport aircraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/19920004713 |
| 著者（英） | Trifu, O.; Savu, G. |
| 著者所属（英） | Aviation Inst. |
| 発行日 | 1991-01-01 |
| 言語 | eng |
| 内容記述 | An aerodynamic optimization procedure developed to minimize the drag to lift ratio of an aircraft configuration: wing - body - tail, in accordance with engineering restrictions, is described. An algorithm developed to search a hypersurface with 18 dimensions, which define an aircraft configuration, is discussed. The results, when considered from the aerodynamic point of view, indicate the optimal configuration is one that combines a lifting fuselage with a canard. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 92N13931 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/129518 |
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