| タイトル | The Minimum Induced Drag of Aerofoils |
| 本文（外部サイト） | http://hdl.handle.net/2060/19800006779 |
| 著者（英） | Munk, M. M. |
| 著者所属（英） | National Advisory Committee for Aeronautics. Ames Aeronautical Lab. |
| 発行日 | 1979-12-01 |
| 言語 | eng |
| 内容記述 | Equations are derived to demonstrate which distribution of lifting elements result in a minimum amount of aerodynamic drag. The lifting elements were arranged (1) in one line, (2) parallel lying in a transverse plane, and (3) in any direction in a transverse plane. It was shown that the distribution of lift which causes the least drag is reduced to the solution of the problem for systems of airfoils which are situated in a plane perpendicular to the direction of flight. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 80N15038
NACA-TR-121 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/568907 |
