| タイトル | A simple approximation method for obtaining the spanwise lift distribution |
| 本文（外部サイト） | http://hdl.handle.net/2060/19930094469 |
| 著者（英） | Schrenk, O |
| 著者所属（英） | National Advisory Committee for Aeronautics |
| 発行日 | 1940-08-01 |
| 言語 | eng |
| 内容記述 | The approximation method described makes possible lift-distribution computations in a few minutes. Comparison with an exact method shows satisfactory agreement. The method is of greater applicability than the exact method and includes also the important case of the wing with end plates. |
| レポートNO | 93R23389
NACA-TM-948 |
| 権利 | No Copyright |
