| タイトル | Design charts relating to the stalling of tapered wings |
| 本文（外部サイト） | http://hdl.handle.net/2060/19930091780 |
| 著者（英） | Anderson, R F; Soule, H A |
| 著者所属（英） | National Advisory Committee for Aeronautics. Langley Aeronautical Lab. |
| 発行日 | 1940-01-01 |
| 言語 | eng |
| 内容記述 | An aid in airplane design, charts have been prepared to show the effects of wing taper, thickness ratio, and Reynolds number on the spanwise location of the initial stalling point. Means of improving poor stalling characteristics resulting from certain combinations of the variables have also been considered; additional figures illustrate the influence of camber increase to the wing tips, washout, central sharp leading edges, and wing-tip slots on the stalling characteristics. Data are included from which the drag increases resulting from the use of these means can be computed. The application of the data to a specific problem is illustrated by an example. |
| レポートNO | 93R21070
NACA-TR-703 |
| 権利 | No Copyright |
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